Skip to main content

2016 | OriginalPaper | Buchkapitel

Expansion Tubes in Australia

verfasst von : David E. Gildfind, Richard G. Morgan, Peter A. Jacobs

Erschienen in: Experimental Methods of Shock Wave Research

Verlag: Springer International Publishing

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

Expansion tubes are hypersonic impulse facilities which are able to produce chemically correct, high enthalpy test flows. They are ideally suited to reproducing super-orbital flight through different atmospheres, and provide an increasingly important tool for aerothermodynamic studies of planetary entry vehicles. Furthermore, their uniquely high total pressure capability makes them the only class of facility currently able to reproduce the free-stream total pressures associated with high Mach number scramjet powered access-to-space. In 1987 The University of Queensland was the first research group to use a free-piston driver to power an expansion tube, and presently operates two such facilities, X2 and X3. While the free-piston driver can maximise the performance of the expansion tube, this mode of operation relies on complex flow processes, provides short test duration, and raises many other challenges in terms of test flow characterisation, instrumentation, and so forth. In the process of developing its own facilities, The University of Queensland has identified and addressed many of these challenges, and in X2 and X3 it has established high performance and reliable capabilities for routine ground testing at hypersonic flight conditions.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literatur
1.
Zurück zum Zitat Stalker, R.J.: Isentropic compression of shock tube driver gas. ARS J. 30, 564 (1960) Stalker, R.J.: Isentropic compression of shock tube driver gas. ARS J. 30, 564 (1960)
2.
Zurück zum Zitat Paull, A., Stalker, R.J.: Scramjet testing in the T3 and T4 hypersonic impulse facilities. In: Curran, E.T., Murthy, S.N.B. (eds.) Scramjet Propulsion, Progress in Astronautics and Aeronautics, pp. 1–46. AIAA, Reston, Virginia (2000) Paull, A., Stalker, R.J.: Scramjet testing in the T3 and T4 hypersonic impulse facilities. In: Curran, E.T., Murthy, S.N.B. (eds.) Scramjet Propulsion, Progress in Astronautics and Aeronautics, pp. 1–46. AIAA, Reston, Virginia (2000)
3.
Zurück zum Zitat Stalker, R.J., Morgan, R.G.: The University of Queensland free piston shock tunnel T4: initial operation and preliminary calibration. In: Proceedings of the 4th National Space Engineering Symposium, IEAust, Adelaide (1988) Stalker, R.J., Morgan, R.G.: The University of Queensland free piston shock tunnel T4: initial operation and preliminary calibration. In: Proceedings of the 4th National Space Engineering Symposium, IEAust, Adelaide (1988)
5.
Zurück zum Zitat Resler, E.L., Bloxsom, D.E.: Very High Mach Number Flows by Unsteady Flow Principles. Cornell University Graduate School of Aeronautical Engineering, Limited Distribution Monograph, Jan 1952 Resler, E.L., Bloxsom, D.E.: Very High Mach Number Flows by Unsteady Flow Principles. Cornell University Graduate School of Aeronautical Engineering, Limited Distribution Monograph, Jan 1952
6.
Zurück zum Zitat Trimpi, R.L.: A preliminary theoretical study of the expansion tube, a new device for producing high-enthalpy short-duration hypersonic gas flows. NASA Technical Report R-133 (1962) Trimpi, R.L.: A preliminary theoretical study of the expansion tube, a new device for producing high-enthalpy short-duration hypersonic gas flows. NASA Technical Report R-133 (1962)
7.
Zurück zum Zitat Trimpi, R.L.: A theoretical Investigation of Simulation in Expansion Tubes and Tunnels. NASA TR R-243, NASA Langley Research Centre, Langley Station, Hampton, VA (1966) Trimpi, R.L.: A theoretical Investigation of Simulation in Expansion Tubes and Tunnels. NASA TR R-243, NASA Langley Research Centre, Langley Station, Hampton, VA (1966)
8.
Zurück zum Zitat Paull, A., Stalker, R.J., Stringer, I.: Experiments on an expansion tube with a free piston driver. In: Proceedings of the AIAA 15th Aerodynamic Testing Conference, AIAA paper 88-2018, San Diego, CA, 18–20 May 1988 Paull, A., Stalker, R.J., Stringer, I.: Experiments on an expansion tube with a free piston driver. In: Proceedings of the AIAA 15th Aerodynamic Testing Conference, AIAA paper 88-2018, San Diego, CA, 18–20 May 1988
9.
Zurück zum Zitat Miller, C.G., Jones, J.J.: Development and performance of the NASA Langley Research Center expansion tube/tunnel, a hypersonic-hypervelocity real-gas facility. In: Archer, R.D., Milton, B.E. (eds.) Proceedings of the 14th International Symposium on Shock Waves, pp. 363–373. Sydney, Australia, Aug 1983 Miller, C.G., Jones, J.J.: Development and performance of the NASA Langley Research Center expansion tube/tunnel, a hypersonic-hypervelocity real-gas facility. In: Archer, R.D., Milton, B.E. (eds.) Proceedings of the 14th International Symposium on Shock Waves, pp. 363–373. Sydney, Australia, Aug 1983
10.
Zurück zum Zitat Miller, C.G.: Operational Experience in the Langley Expansion Tube With Various Test Gases. NASA Technical Memorandum 78637, NASA Langley Research Center, Hampton, VA, Dec 1977 Miller, C.G.: Operational Experience in the Langley Expansion Tube With Various Test Gases. NASA Technical Memorandum 78637, NASA Langley Research Center, Hampton, VA, Dec 1977
11.
Zurück zum Zitat Paull, A., Stalker, R.J.: Test flow disturbances in an expansion tube. J. Fluid Mech. 245, 493–521 (1992)CrossRef Paull, A., Stalker, R.J.: Test flow disturbances in an expansion tube. J. Fluid Mech. 245, 493–521 (1992)CrossRef
12.
Zurück zum Zitat Stalker, R.J.: Recent developments with free piston drivers. In: Kim, Y.W. (ed.) Current topics in shock waves 17th International Symposium on Shock Waves and Shock Tubes, pp 96–105. Bethlehem, PA (1990) Stalker, R.J.: Recent developments with free piston drivers. In: Kim, Y.W. (ed.) Current topics in shock waves 17th International Symposium on Shock Waves and Shock Tubes, pp 96–105. Bethlehem, PA (1990)
13.
Zurück zum Zitat Paull, A., Stalker, R.J.: The effect of an acoustic wave as it traverses an unsteady expansion. Phys. Fluids 3(4), 717–719 (1991)CrossRef Paull, A., Stalker, R.J.: The effect of an acoustic wave as it traverses an unsteady expansion. Phys. Fluids 3(4), 717–719 (1991)CrossRef
14.
Zurück zum Zitat Bakos, R.J., Erdos, J.I.: Options for enhancement of the performance of shock-expansion tubes and tunnels. In: Proceedings of the 33rd Aerospace Sciences Meeting and Exhibit, AIAA 95-0799, Reno, NV, 9–12 Jan 1995 Bakos, R.J., Erdos, J.I.: Options for enhancement of the performance of shock-expansion tubes and tunnels. In: Proceedings of the 33rd Aerospace Sciences Meeting and Exhibit, AIAA 95-0799, Reno, NV, 9–12 Jan 1995
15.
Zurück zum Zitat Morgan, R.G.: Free-piston driven expansion tubes. In: Ben-Dor, G., Igra, O., Elperin, T. (eds.) Handbook of Shock Waves, vol. 1, pp. 603–622. Academic Press, New York (2001) Morgan, R.G.: Free-piston driven expansion tubes. In: Ben-Dor, G., Igra, O., Elperin, T. (eds.) Handbook of Shock Waves, vol. 1, pp. 603–622. Academic Press, New York (2001)
16.
Zurück zum Zitat Bakos, R.J., Morgan, R.G., Tamagno, J.: Effects of oxygen dissociation on hypervelocity combustion experiments. In: Proceedings of the AIAA 17th Aerospace Ground Testing Conference, AIAA-92-3964, Nashville, TN, 6–8 July 1992 Bakos, R.J., Morgan, R.G., Tamagno, J.: Effects of oxygen dissociation on hypervelocity combustion experiments. In: Proceedings of the AIAA 17th Aerospace Ground Testing Conference, AIAA-92-3964, Nashville, TN, 6–8 July 1992
17.
Zurück zum Zitat Jones, J.J.: Some performance characteristics of the LRC 3-3/4-inch pilot expansion tube using an unheated hydrogen driver. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp 7–26. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965 Jones, J.J.: Some performance characteristics of the LRC 3-3/4-inch pilot expansion tube using an unheated hydrogen driver. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp 7–26. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965
18.
Zurück zum Zitat Spurk, J.H.: Design, operation, and preliminary results of the BLR expansion tube. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp. 111–144. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965 Spurk, J.H.: Design, operation, and preliminary results of the BLR expansion tube. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp. 111–144. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965
19.
Zurück zum Zitat Norfleet, G.D., Lacey, J.J., Whitfield, J.D.: Results of an experimental investigation of the performance characteristics of an expansion tube. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp. 49–110. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965 Norfleet, G.D., Lacey, J.J., Whitfield, J.D.: Results of an experimental investigation of the performance characteristics of an expansion tube. In: Proceedings of the Fourth Hypervelocity Techniques Symposium, pp. 49–110. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee, 15–16 Nov 1965
20.
Zurück zum Zitat Miller, C.G.: Operational experience in the Langley expansion tube with various test gases. NASA Technical Memorandum 78637 (1977) Miller, C.G.: Operational experience in the Langley expansion tube with various test gases. NASA Technical Memorandum 78637 (1977)
21.
Zurück zum Zitat Jacobs, P.A.: Numerical simulation of transient hypervelocity flow in an expansion tube. ICASE Interim Report 20/NASA Contractor Report 189601, Langley Research Center, Hampton, Virginia, Jan 1992 Jacobs, P.A.: Numerical simulation of transient hypervelocity flow in an expansion tube. ICASE Interim Report 20/NASA Contractor Report 189601, Langley Research Center, Hampton, Virginia, Jan 1992
22.
Zurück zum Zitat Neely, A.J., Stalker, R.J., Paull, A.: High enthalpy, hypervelocity flows of air and argon in an expansion tube. Aeronaut. J. 95(946), 175–186 (1991) Neely, A.J., Stalker, R.J., Paull, A.: High enthalpy, hypervelocity flows of air and argon in an expansion tube. Aeronaut. J. 95(946), 175–186 (1991)
23.
Zurück zum Zitat Jacobs, P.A.: Numerical simulation of transient hypervelocity flow in an expansion tube. Comput. Fluids 23(1), 77–101 (1994)CrossRef Jacobs, P.A.: Numerical simulation of transient hypervelocity flow in an expansion tube. Comput. Fluids 23(1), 77–101 (1994)CrossRef
24.
Zurück zum Zitat Henshall, B.D.: The use of multiple diaphragms in shock tubes. A.R.C. Technical Report C.P. No. 291, Ministry of Supply, Aeronautical Research Council (1956) Henshall, B.D.: The use of multiple diaphragms in shock tubes. A.R.C. Technical Report C.P. No. 291, Ministry of Supply, Aeronautical Research Council (1956)
25.
Zurück zum Zitat Stalker, R.J., Plumb, D.L.: Diaphragm-type shock tube for high shock speeds. Nature 218(5143), 789–790 (1968)CrossRef Stalker, R.J., Plumb, D.L.: Diaphragm-type shock tube for high shock speeds. Nature 218(5143), 789–790 (1968)CrossRef
26.
Zurück zum Zitat Morgan, R.G.: A review of the use of expansion tubes for creating superorbital flows. In: Proceedings of the 35th Aerospace Sciences Meeting and Exhibit, AIAA 97-0279, Reno, NV, 6–10 Jan 1997 Morgan, R.G.: A review of the use of expansion tubes for creating superorbital flows. In: Proceedings of the 35th Aerospace Sciences Meeting and Exhibit, AIAA 97-0279, Reno, NV, 6–10 Jan 1997
27.
Zurück zum Zitat Morgan, R.G., Stalker, R.J.: Double diaphragm driven free piston expansion tube. In: Proceedings of the 18th International Symposium on Shock Waves, Sendai, Japan, 21–26 July 1991 Morgan, R.G., Stalker, R.J.: Double diaphragm driven free piston expansion tube. In: Proceedings of the 18th International Symposium on Shock Waves, Sendai, Japan, 21–26 July 1991
28.
Zurück zum Zitat Neely, A.J., Morgan, R.G.: The superorbital expansion tube concept, experiment and analysis. Aeronaut. J. 98, 97–105 (1994) Neely, A.J., Morgan, R.G.: The superorbital expansion tube concept, experiment and analysis. Aeronaut. J. 98, 97–105 (1994)
29.
Zurück zum Zitat Scott, M.P., Morgan, R.G., Jacobs, P.A.: A new single stage driver for the X2 expansion tube. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibition, AIAA-2005-697, Reno, Nevada, 10–13 Jan 2005 Scott, M.P., Morgan, R.G., Jacobs, P.A.: A new single stage driver for the X2 expansion tube. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibition, AIAA-2005-697, Reno, Nevada, 10–13 Jan 2005
30.
Zurück zum Zitat Doolan, C.J., Morgan, R.G.: A two-stage free-piston driver. Shock Waves 9(4), 239–249 (1999)CrossRef Doolan, C.J., Morgan, R.G.: A two-stage free-piston driver. Shock Waves 9(4), 239–249 (1999)CrossRef
31.
Zurück zum Zitat Doolan, C., Morgan, R.G.: Test-time optimization of a large scale hypervelocity expansion tunnel. In: Proceedings of the Eighth National Space Engineering Symposium, The Institution of Engineers, Australia, Brisbane, 20–21 Sept 1993 Doolan, C., Morgan, R.G.: Test-time optimization of a large scale hypervelocity expansion tunnel. In: Proceedings of the Eighth National Space Engineering Symposium, The Institution of Engineers, Australia, Brisbane, 20–21 Sept 1993
32.
Zurück zum Zitat Eichmann, T.N., McIntyre, T.J., Bishop, A.I., Vakata, S., Rubinsztein-Dunlop, H.: Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders. Shock Waves 16, 299–307 (2007) Eichmann, T.N., McIntyre, T.J., Bishop, A.I., Vakata, S., Rubinsztein-Dunlop, H.: Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders. Shock Waves 16, 299–307 (2007)
33.
Zurück zum Zitat McIntyre, T.J., Lourel, I., Eichmann, T.N., Morgan, R.G., Jacobs, P.A., Bishop, A.I.: Experimental expansion tube study of the flow over a toroidal ballute. J. Spacecraft Rockets 41(5), 716–725 (2004)CrossRef McIntyre, T.J., Lourel, I., Eichmann, T.N., Morgan, R.G., Jacobs, P.A., Bishop, A.I.: Experimental expansion tube study of the flow over a toroidal ballute. J. Spacecraft Rockets 41(5), 716–725 (2004)CrossRef
34.
Zurück zum Zitat Littleton, B.N., Bishop, A.I., McIntyre, T.J., Barker, P.F., Rubinsztein-Dunlop, H.: Flow tagging velocimetry in a superorbital expansion tube. Shock Waves 10, 225–228 (2000) Littleton, B.N., Bishop, A.I., McIntyre, T.J., Barker, P.F., Rubinsztein-Dunlop, H.: Flow tagging velocimetry in a superorbital expansion tube. Shock Waves 10, 225–228 (2000)
35.
Zurück zum Zitat Hayne, M.J., Mee, D.J., Gai, S.L., McIntyre, T.J.: Boundary layers on a flat plate at sub- and superorbital speeds. J. Thermophys. Heat Transfer 21(4), 772–779 (2007)CrossRef Hayne, M.J., Mee, D.J., Gai, S.L., McIntyre, T.J.: Boundary layers on a flat plate at sub- and superorbital speeds. J. Thermophys. Heat Transfer 21(4), 772–779 (2007)CrossRef
36.
Zurück zum Zitat Higgins, C., Inger, G.R., Morgan, R., Eichmann, T., McIntyre, T.: Shock standoff on hypersonic blunt bodies in multi-temperature ionizing nonequilibrium gas flows. In: Proceedings of the 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, St Louis, Missouri, 24–26 June 2002 Higgins, C., Inger, G.R., Morgan, R., Eichmann, T., McIntyre, T.: Shock standoff on hypersonic blunt bodies in multi-temperature ionizing nonequilibrium gas flows. In: Proceedings of the 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, St Louis, Missouri, 24–26 June 2002
37.
Zurück zum Zitat Eichmann, T.N.: Radiation measurements in a simulated Mars atmosphere. PhD Thesis, School of Mathematics and Physics, The University of Queensland, Brisbane, Australia (2012) Eichmann, T.N.: Radiation measurements in a simulated Mars atmosphere. PhD Thesis, School of Mathematics and Physics, The University of Queensland, Brisbane, Australia (2012)
38.
Zurück zum Zitat Jacobs, C.M.: Radiation in low density hypervelocity flows. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland, Brisbane, Australia (2011) Jacobs, C.M.: Radiation in low density hypervelocity flows. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland, Brisbane, Australia (2011)
39.
Zurück zum Zitat Brandis, A.M., Morgan, R.G., McIntyre, T.J.: Analysis of nonequilibrium CN radiation encountered during Titan atmospheric entry. AIAA J. Thermophys. Heat Transfer 25(4), 493–499 (2007)CrossRef Brandis, A.M., Morgan, R.G., McIntyre, T.J.: Analysis of nonequilibrium CN radiation encountered during Titan atmospheric entry. AIAA J. Thermophys. Heat Transfer 25(4), 493–499 (2007)CrossRef
40.
Zurück zum Zitat McGilvray, M., Morgan, R., Jacobs, P.: Scramjet experiments in an expansion tunnel: evaluated using a quasi-steady analysis technique. AIAA J. 48(8), 1635–1646 (2010)CrossRef McGilvray, M., Morgan, R., Jacobs, P.: Scramjet experiments in an expansion tunnel: evaluated using a quasi-steady analysis technique. AIAA J. 48(8), 1635–1646 (2010)CrossRef
41.
Zurück zum Zitat Gildfind, D.E., Morgan, R.G., McGilvray, M., Jacobs, P.A., Stalker, R.J., Eichmann., T.N.: Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. Shock Waves 21(6), 559–572 (2011) Gildfind, D.E., Morgan, R.G., McGilvray, M., Jacobs, P.A., Stalker, R.J., Eichmann., T.N.: Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. Shock Waves 21(6), 559–572 (2011)
42.
Zurück zum Zitat Jacobs, P.A.: Quasi-one-dimensional modelling of a free-piston shock tunnel. AIAA J. 32(1), 137–145 (1994)CrossRef Jacobs, P.A.: Quasi-one-dimensional modelling of a free-piston shock tunnel. AIAA J. 32(1), 137–145 (1994)CrossRef
43.
Zurück zum Zitat Stalker, R.J.: A study of the free-piston shock tunnel. AIAA J. 5(12), 2160–2165 (1967)CrossRef Stalker, R.J.: A study of the free-piston shock tunnel. AIAA J. 5(12), 2160–2165 (1967)CrossRef
44.
Zurück zum Zitat Itoh, K., Ueda, S., Komuro, T., Sato, K., Takahashi, M., Myajima, H., Tanno, H., Muramoto, H.: Improvement of a free piston driver for a high-enthalpy shock tunnel. Shock Waves 8(4), 215–233 (1998)CrossRef Itoh, K., Ueda, S., Komuro, T., Sato, K., Takahashi, M., Myajima, H., Tanno, H., Muramoto, H.: Improvement of a free piston driver for a high-enthalpy shock tunnel. Shock Waves 8(4), 215–233 (1998)CrossRef
45.
Zurück zum Zitat Gildfind, D.E., Morgan, R.G., Jacobs, P.A., McGilvray, M.: Production of High-Mach-Number scramjet flow conditions in an expansion tube. AIAA J. 52(1), 162–177 (2014)CrossRef Gildfind, D.E., Morgan, R.G., Jacobs, P.A., McGilvray, M.: Production of High-Mach-Number scramjet flow conditions in an expansion tube. AIAA J. 52(1), 162–177 (2014)CrossRef
46.
Zurück zum Zitat Porat, H., Zander, F., Morgan, R.G., McIntyre, T.J.: Emission spectroscopy of a mach disk at Titan atmospheric entry conditions. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013 Porat, H., Zander, F., Morgan, R.G., McIntyre, T.J.: Emission spectroscopy of a mach disk at Titan atmospheric entry conditions. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013
47.
Zurück zum Zitat Sheikh, U.A., Jacobs, C., Laux, C.O., Morgan, R.G., McIntyre, T.J.: Measurements of radiating flow fields in the vacuum ultraviolet. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013 Sheikh, U.A., Jacobs, C., Laux, C.O., Morgan, R.G., McIntyre, T.J.: Measurements of radiating flow fields in the vacuum ultraviolet. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013
48.
Zurück zum Zitat Zander, F., Morgan, R.G., Sheikh, U., Buttsworth, D.R., Teakle, P.R.: Hot-wall reentry testing in hypersonic impulse facilities. AIAA J. 51(2), 476–484 (2013)CrossRef Zander, F., Morgan, R.G., Sheikh, U., Buttsworth, D.R., Teakle, P.R.: Hot-wall reentry testing in hypersonic impulse facilities. AIAA J. 51(2), 476–484 (2013)CrossRef
49.
Zurück zum Zitat James, C.M., Gildfind, D.E., Morgan, R.G., McIntyre, T.J.: Working towards simulating gas giant entry radiation in an expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013 James, C.M., Gildfind, D.E., Morgan, R.G., McIntyre, T.J.: Working towards simulating gas giant entry radiation in an expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin, Madison, 14–19 July 2013
50.
Zurück zum Zitat Gildfind, D.E., James, C.M., Morgan, R.G.: Free-piston driver performance characterisation using experimental shock speeds through helium. Shock Waves, 25(1), 169–176 (2015) Gildfind, D.E., James, C.M., Morgan, R.G.: Free-piston driver performance characterisation using experimental shock speeds through helium. Shock Waves, 25(1), 169–176 (2015)
51.
Zurück zum Zitat Bakos, R.J., Calleja, J.F., Erdos, J.I., Auslender, A.H., Sussman, M.A., Wilson, G.J.: Design, calibration and analysis of a tunnel mode of operation for the hypulse facility. In: Proceedings of the 19th AIAA Advanced Measurement and Ground Testing Technology Conference, AIAA 96-2194, New Orleans, LA, 17–20 June 1996 Bakos, R.J., Calleja, J.F., Erdos, J.I., Auslender, A.H., Sussman, M.A., Wilson, G.J.: Design, calibration and analysis of a tunnel mode of operation for the hypulse facility. In: Proceedings of the 19th AIAA Advanced Measurement and Ground Testing Technology Conference, AIAA 96-2194, New Orleans, LA, 17–20 June 1996
52.
Zurück zum Zitat Stewart, B.S., Jacobs, P.A., Morgan, R.G.: The starting process of an expansion tube nozzle. In: 23rd International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23–27 July 2001 Stewart, B.S., Jacobs, P.A., Morgan, R.G.: The starting process of an expansion tube nozzle. In: 23rd International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23–27 July 2001
53.
Zurück zum Zitat Chue, R.S.M., Bakos, R.J., Tsai, C.-Y., Betti, A.: Design of a shock-free expansion tunnel nozzle in hypulse. Shock Waves 13(4), 261–270 (2003)CrossRef Chue, R.S.M., Bakos, R.J., Tsai, C.-Y., Betti, A.: Design of a shock-free expansion tunnel nozzle in hypulse. Shock Waves 13(4), 261–270 (2003)CrossRef
54.
Zurück zum Zitat Scott, M.P.: Development and modelling of expansion tubes. PhD Thesis, Centre for Hypersonics, Department of Mechanical Engineering, University of Queensland, Brisbane, Australia (2006) Scott, M.P.: Development and modelling of expansion tubes. PhD Thesis, Centre for Hypersonics, Department of Mechanical Engineering, University of Queensland, Brisbane, Australia (2006)
55.
Zurück zum Zitat Craddock, C.S.: Computational optimization of scramjets and shock tunnel nozzles. PhD Thesis, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (1999) Craddock, C.S.: Computational optimization of scramjets and shock tunnel nozzles. PhD Thesis, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (1999)
56.
Zurück zum Zitat Gildfind, D.: Development of high total pressure scramjet flow conditions using the X2 expansion tube. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2012) Gildfind, D.: Development of high total pressure scramjet flow conditions using the X2 expansion tube. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2012)
57.
Zurück zum Zitat McGilvray, M., Jacobs, P.A., Morgan, R.G., Gollan, R.J., Jacobs, C.M.: Helmholtz resonance of pitot pressure measurements in impulsive hypersonic test facilities. AIAA J. 47(10), 2430–2439 (2009)CrossRef McGilvray, M., Jacobs, P.A., Morgan, R.G., Gollan, R.J., Jacobs, C.M.: Helmholtz resonance of pitot pressure measurements in impulsive hypersonic test facilities. AIAA J. 47(10), 2430–2439 (2009)CrossRef
58.
Zurück zum Zitat Chiu, H.S., Mee, D.J.: Modified bar gauges. Research Report Number 2003/22, Division of Mechanical Engineering, The University of Queensland (2003) Chiu, H.S., Mee, D.J.: Modified bar gauges. Research Report Number 2003/22, Division of Mechanical Engineering, The University of Queensland (2003)
59.
Zurück zum Zitat Wheatley, V., Chiu, H.S., Jacobs, P.A., Macrossan, M.N., Mee, D.J., Morgan, R.G.: Rarefied, superorbital flows in an expansion tube. Int. J. Numer. Meth. Heat Fluid Flow 14(4), 512–537 (2004)CrossRef Wheatley, V., Chiu, H.S., Jacobs, P.A., Macrossan, M.N., Mee, D.J., Morgan, R.G.: Rarefied, superorbital flows in an expansion tube. Int. J. Numer. Meth. Heat Fluid Flow 14(4), 512–537 (2004)CrossRef
60.
Zurück zum Zitat Hillier, R., Boyce, R.R., Creighton, S.A., Fiala, A., Jackson, A.P., Mallinson, S.G., Sheikh, A.H., Soltani, S., Williams, S.: Development of some hypersonic benchmark flows using CFD and experiment. Shock Waves 12(5), 375–384 (2003)CrossRef Hillier, R., Boyce, R.R., Creighton, S.A., Fiala, A., Jackson, A.P., Mallinson, S.G., Sheikh, A.H., Soltani, S., Williams, S.: Development of some hypersonic benchmark flows using CFD and experiment. Shock Waves 12(5), 375–384 (2003)CrossRef
61.
Zurück zum Zitat Roy, C.J., Oberkampf, W.L., McWherter-Payne, M.A.: Verification and validation for laminar hypersonic flow fields, Part 2: validation. AIAA J. 41(10), 1944–1954 (2003)CrossRef Roy, C.J., Oberkampf, W.L., McWherter-Payne, M.A.: Verification and validation for laminar hypersonic flow fields, Part 2: validation. AIAA J. 41(10), 1944–1954 (2003)CrossRef
62.
Zurück zum Zitat Anderson, G., Kumar, A., Erdos, J.: Progress in hypersonic combustion technology with computation and experiment. In: AIAA Second International Aerospace Planes Conference, AIAA-90-5254, Orlando, FL, 29–31 Oct 1990 Anderson, G., Kumar, A., Erdos, J.: Progress in hypersonic combustion technology with computation and experiment. In: AIAA Second International Aerospace Planes Conference, AIAA-90-5254, Orlando, FL, 29–31 Oct 1990
63.
Zurück zum Zitat Anderson, G.Y., McClinton, C.R., Weidner, J.P.: Scramjet performance. In: Curran, E.T., Murthy, S.N.B. (eds.) Scramjet Propulsion, Progress in Astronautics and Aeronautics, pp. 369–446. AIAA, Reston, Virginia (2000) Anderson, G.Y., McClinton, C.R., Weidner, J.P.: Scramjet performance. In: Curran, E.T., Murthy, S.N.B. (eds.) Scramjet Propulsion, Progress in Astronautics and Aeronautics, pp. 369–446. AIAA, Reston, Virginia (2000)
64.
Zurück zum Zitat Candler, G.V., Nompelis, I.: CFD validation for hypersonic flight: real gas flows. In: Proceedings of the 40th AIAA Aerospace Sciences Meeting and Exhibit, RTO-TR-AVT-007-V3/AIAA 2002-0434, Reno, NV, 14–17 Jan 2002 Candler, G.V., Nompelis, I.: CFD validation for hypersonic flight: real gas flows. In: Proceedings of the 40th AIAA Aerospace Sciences Meeting and Exhibit, RTO-TR-AVT-007-V3/AIAA 2002-0434, Reno, NV, 14–17 Jan 2002
65.
Zurück zum Zitat Marvin, J.G.: A CFD Validation Roadmap for Hypersonic Flows. NASA Technical Memorandum 103935, Ames Research Center, Moffett Field, California (1992) Marvin, J.G.: A CFD Validation Roadmap for Hypersonic Flows. NASA Technical Memorandum 103935, Ames Research Center, Moffett Field, California (1992)
66.
Zurück zum Zitat Jacobs, P.A., Gollan, R.J.: The Eilmer3 Code: User Guide and Example Book. Mechanical Engineering Report 2008/07, Department of Mechanical and Mining Engineering, The University of Queensland (2009) Jacobs, P.A., Gollan, R.J.: The Eilmer3 Code: User Guide and Example Book. Mechanical Engineering Report 2008/07, Department of Mechanical and Mining Engineering, The University of Queensland (2009)
67.
Zurück zum Zitat Jacobs, P.A., Gollan, R.J., Denman, A.J., O’Flaherty, B.T., Potter, D.F., Petrie-Repar, P.J., Johnston, I.A.: Eilmer’s Theory Book: Basic Models for Gas Dynamics and Thermochemistry. Mechanical Engineering Report 2010/09, Department of Mechanical and Mining Engineering, The University of Queensland (2010) Jacobs, P.A., Gollan, R.J., Denman, A.J., O’Flaherty, B.T., Potter, D.F., Petrie-Repar, P.J., Johnston, I.A.: Eilmer’s Theory Book: Basic Models for Gas Dynamics and Thermochemistry. Mechanical Engineering Report 2010/09, Department of Mechanical and Mining Engineering, The University of Queensland (2010)
68.
Zurück zum Zitat Gollan, R.J., Jacobs, P.A.: About the formulation, verification and validation of the hypersonic flow solver Eilmer. Int. J. Numer. Meth. Fluids 73, 19–57 (2013)MathSciNetCrossRef Gollan, R.J., Jacobs, P.A.: About the formulation, verification and validation of the hypersonic flow solver Eilmer. Int. J. Numer. Meth. Fluids 73, 19–57 (2013)MathSciNetCrossRef
69.
Zurück zum Zitat Potter, D.F., Gollan, R.J., Eichmann, T., McIntyre, T.J., Morgan, R.G., Jacobs, P.A.: Simulation of CO2-N2 expansion tunnel flows for the study of radiating shock layers. In: Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2008-1280, Reno, Nevada, 7–10 Jan 2008 Potter, D.F., Gollan, R.J., Eichmann, T., McIntyre, T.J., Morgan, R.G., Jacobs, P.A.: Simulation of CO2-N2 expansion tunnel flows for the study of radiating shock layers. In: Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2008-1280, Reno, Nevada, 7–10 Jan 2008
70.
Zurück zum Zitat Morgan, R.G., McIntyre, T.J., Jacobs, P.A., Buttsworth, D.R., Macrossan, M.N., Gollan, R.J., Capra, B.R., Brandis, A.M., Potter, P., Eichmann, T., Jacobs, C.M., McGilvray, M., van Diem, D., Scott, M.P.: Impulse facility simulation of hypervelocity radiating flows. In: Proceedings of the 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 6–8 Sept, Rome, Italy. ESA Publication, Noordwijk, The Netherlands, Nov 2006 Morgan, R.G., McIntyre, T.J., Jacobs, P.A., Buttsworth, D.R., Macrossan, M.N., Gollan, R.J., Capra, B.R., Brandis, A.M., Potter, P., Eichmann, T., Jacobs, C.M., McGilvray, M., van Diem, D., Scott, M.P.: Impulse facility simulation of hypervelocity radiating flows. In: Proceedings of the 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 6–8 Sept, Rome, Italy. ESA Publication, Noordwijk, The Netherlands, Nov 2006
71.
Zurück zum Zitat Jacobs, P.A., Silvester, T.B., Morgan, R.G., Scott, M.P., Gollan, R.G., McIntyre, T.J.: Superorbital expansion tube operation: estimates of flow conditions via numerical simulation. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting, AIAA-2005-0694, Reno, NV, 10–13 Jan 2005 Jacobs, P.A., Silvester, T.B., Morgan, R.G., Scott, M.P., Gollan, R.G., McIntyre, T.J.: Superorbital expansion tube operation: estimates of flow conditions via numerical simulation. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting, AIAA-2005-0694, Reno, NV, 10–13 Jan 2005
72.
Zurück zum Zitat Wendt, M., Macrossan, M., Jacobs, P., Mee, D.: Pilot study for a rarefied hypervelocity test facility. In: Proceedings of the 13th Australasian Fluid Mechanics Conference, Monash University, Melbourne, Australia, 13–18 Dec 1998 Wendt, M., Macrossan, M., Jacobs, P., Mee, D.: Pilot study for a rarefied hypervelocity test facility. In: Proceedings of the 13th Australasian Fluid Mechanics Conference, Monash University, Melbourne, Australia, 13–18 Dec 1998
73.
Zurück zum Zitat McGilvray, M., Austin, J.M., Sharma, M., Jacobs, P.A., Morgan, R.G.: Diagnostic modelling of an expansion tube operating condition. Shock Waves 19(1), 59–66 (2009)CrossRef McGilvray, M., Austin, J.M., Sharma, M., Jacobs, P.A., Morgan, R.G.: Diagnostic modelling of an expansion tube operating condition. Shock Waves 19(1), 59–66 (2009)CrossRef
74.
Zurück zum Zitat Stewart, B., Morgan, R.G., Jacobs, P.A., Hayne, M.: Flow establishment in large-scale high-performance expansion tubes. In: Proceedings of the AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Paper No. 5239, Orleans, France, 29 Sept–4 Oct 2002 Stewart, B., Morgan, R.G., Jacobs, P.A., Hayne, M.: Flow establishment in large-scale high-performance expansion tubes. In: Proceedings of the AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Paper No. 5239, Orleans, France, 29 Sept–4 Oct 2002
75.
Zurück zum Zitat Gollan, R.J., Jacobs, C.M., Jacobs, P.A., Morgan, R.G., McIntyre, T.J., Macrossan, M.N., Buttsworth, D.R., Eichmann, T.N., Potter, D.F.: A simulation technique for radiating shock tube flows. In: Klauss, H., Seiler, F. (eds.) Proceedings of the 26th International Symposium on Shock Waves, pp. 465–470. Göttingen, Germany, 15–20 July 2007 Gollan, R.J., Jacobs, C.M., Jacobs, P.A., Morgan, R.G., McIntyre, T.J., Macrossan, M.N., Buttsworth, D.R., Eichmann, T.N., Potter, D.F.: A simulation technique for radiating shock tube flows. In: Klauss, H., Seiler, F. (eds.) Proceedings of the 26th International Symposium on Shock Waves, pp. 465–470. Göttingen, Germany, 15–20 July 2007
76.
Zurück zum Zitat Gildfind, D.E., Sancho, J., Morgan, R.G.: High Mach number scramjet test flows in the X3 expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin-Madison, Memorial Union, 14–19 July 2013 Gildfind, D.E., Sancho, J., Morgan, R.G.: High Mach number scramjet test flows in the X3 expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin-Madison, Memorial Union, 14–19 July 2013
77.
Zurück zum Zitat Gollan, R.J.: The computational modelling of high-temperature gas effects with application to hypersonic flows. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2008) Gollan, R.J.: The computational modelling of high-temperature gas effects with application to hypersonic flows. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2008)
78.
Zurück zum Zitat Potter, D.: Modelling of radiating shock layers for atmospheric entry at Earth and Mars. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2011) Potter, D.: Modelling of radiating shock layers for atmospheric entry at Earth and Mars. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane, Australia (2011)
79.
Zurück zum Zitat McGilvray, M.: The use of expansion tube facilities for scramjet testing. PhD Thesis, Centre for Hypersonics, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (2008) McGilvray, M.: The use of expansion tube facilities for scramjet testing. PhD Thesis, Centre for Hypersonics, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (2008)
80.
Zurück zum Zitat Capra, B.R., Morgan, R.G.: Radiative and total heat transfer measurements to a Titan explorer model. J. Spacecraft Rockets 49(1) (2012) Capra, B.R., Morgan, R.G.: Radiative and total heat transfer measurements to a Titan explorer model. J. Spacecraft Rockets 49(1) (2012)
81.
Zurück zum Zitat Davey, M.G.: A hypersonic nozzle for the X3 expansion tube. Bachelor of Engineering Thesis, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (2006) Davey, M.G.: A hypersonic nozzle for the X3 expansion tube. Bachelor of Engineering Thesis, Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (2006)
82.
Zurück zum Zitat Jacobs, P.A., Stalker, R.J.: Design of axisymmetric nozzles for reflected shock tunnels. Report 1/89, Department of Mechanical Engineering, University of Queensland (1989) Jacobs, P.A., Stalker, R.J.: Design of axisymmetric nozzles for reflected shock tunnels. Report 1/89, Department of Mechanical Engineering, University of Queensland (1989)
83.
Zurück zum Zitat Hass, N.E., Shih, A.T., Rogers, R.C.: Mach 12 and 15 scramjet test capabilities of the hypulse shock-expansion tunnel. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2005-690, Reno, Nevada, 10–13 Jan 2005 Hass, N.E., Shih, A.T., Rogers, R.C.: Mach 12 and 15 scramjet test capabilities of the hypulse shock-expansion tunnel. In: Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2005-690, Reno, Nevada, 10–13 Jan 2005
84.
Zurück zum Zitat Gildfind, D.E., Morgan, R.G., Sancho, J.: Design and commissioning of a new lightweight piston for the X3 expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin-Madison, Memorial Union, 14–19 July 2013 Gildfind, D.E., Morgan, R.G., Sancho, J.: Design and commissioning of a new lightweight piston for the X3 expansion tube. In: Proceedings of the 29th International Symposium on Shock Waves, University of Wisconsin-Madison, Memorial Union, 14–19 July 2013
85.
Zurück zum Zitat Pinckney, S.Z.: A short static-pressure probe design for supersonic flow. NASA TN D-7978 (1975) Pinckney, S.Z.: A short static-pressure probe design for supersonic flow. NASA TN D-7978 (1975)
86.
Zurück zum Zitat Zander, F.: Personal communication (2012) Zander, F.: Personal communication (2012)
87.
Zurück zum Zitat McGilvray, M., Kirchhartz, R., Jazra, T.: Comparison of Mach 10 scramjet measurements from different impulse facilities. AIAA J. 48(8), 1647–1651 (2010)CrossRef McGilvray, M., Kirchhartz, R., Jazra, T.: Comparison of Mach 10 scramjet measurements from different impulse facilities. AIAA J. 48(8), 1647–1651 (2010)CrossRef
Metadaten
Titel
Expansion Tubes in Australia
verfasst von
David E. Gildfind
Richard G. Morgan
Peter A. Jacobs
Copyright-Jahr
2016
DOI
https://doi.org/10.1007/978-3-319-23745-9_13

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.