Skip to main content
Top

2018 | OriginalPaper | Chapter

Calibration of Fast-Response Temperature Sensitive Paints for Their Application in Hypersonic High Enthalpy Flows

Authors : Jan Martinez Schramm, Frank Edzards, Klaus Hannemann

Published in: New Results in Numerical and Experimental Fluid Mechanics XI

Publisher: Springer International Publishing

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

For a spacecraft traveling at hypersonic speeds, the design of the vehicle’s thermal protection system is crucial [2] and the accurate quantification of the surface heat flux is mandatory to aid this design. Traditional surface-mounted temperature sensors, such as thermocouples and thin film gauges, have been widely used as reported already over 40 years ago by [19]. These sensors have response times on the order of a few microseconds, and thus data can be sampled with high temporal resolution; typically 1 MHz. However, the spatial resolution is less satisfactory: the packing density is limited by the sensor size and a great amount of expertise is needed to mount sensors on narrow geometries (e.g. sharp leading edges or corners). In addition, the installation of large numbers of transducers results in complicated wiring and high costs. The clear advantages of temperature sensitive paints (TSPs) over the classical techniques are the non-intrusive measurement approach and the high spatial resolution. A feasibility application of fast-response TSPs in Europe’s major hypersonic facility, the High Enthalpy Shock Tunnel Göttingen (HEG), on transition measurements has already been published [18]. These measurements demonstrated the ability of the TSP method to be used for measurements of time resolved surface temperatures and consequently the determination of surface heat fluxes; the TSP used in the publication was based on the luminophore Ru(phen). This paper will discuss the prerequisites, the requirements and the calibration work which has to be accomplished to progress the development of ultra-fast temperature sensitive paints towards a more versatile application in hypersonic high enthalpy flows in the HEG. Additional information on the HEG is reported by Hannemann and Martinez Schramm [7]. The calibration procedure is shown for the laser dye 4-Methylumbelliferone (4MU) which has been determined to be the next promising candidate for the application in the HEG [15].

Dont have a licence yet? Then find out more about our products and how to get one now:

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!

Literature
1.
go back to reference Beck, W., Klein, C., Henne, U., Sachs, W., Martinez Schramm, J., Wagner, A., Hannemann, K., Gawehn, T., Gülhan, A.: Application of temperature and pressure sensitive paints to DLR Hypersonic facilities: lessons learned. In: 53rd AIAA Aerospace Sciences Meeting, AIAA Science and Technology Forum 2015, Paper 2015-0023, 5-9. Januar: Kissimmee. Florida, USA (2015) Beck, W., Klein, C., Henne, U., Sachs, W., Martinez Schramm, J., Wagner, A., Hannemann, K., Gawehn, T., Gülhan, A.: Application of temperature and pressure sensitive paints to DLR Hypersonic facilities: lessons learned. In: 53rd AIAA Aerospace Sciences Meeting, AIAA Science and Technology Forum 2015, Paper 2015-0023, 5-9. Januar: Kissimmee. Florida, USA (2015)
3.
go back to reference Cai, Z., Liu, T., Wang, B., Rubal, J., Sullivan, J.P.: Numerical inverse heat transfer analysis for temperature-sensitive-paint measurement in hypersonic tunnels. J Thermophys. Heat Tran. 25(1), 59–67 (2011) Cai, Z., Liu, T., Wang, B., Rubal, J., Sullivan, J.P.: Numerical inverse heat transfer analysis for temperature-sensitive-paint measurement in hypersonic tunnels. J Thermophys. Heat Tran. 25(1), 59–67 (2011)
4.
go back to reference Cook, W.J., Felderman, E.J.: Reduction of data from thin-film heat transfer gage: a concise numerical technique. AIAA J. 4(3), 561–562 (1966)CrossRef Cook, W.J., Felderman, E.J.: Reduction of data from thin-film heat transfer gage: a concise numerical technique. AIAA J. 4(3), 561–562 (1966)CrossRef
5.
go back to reference Dunn, M.G., Geroge, W.K., Rae, W.J., Woodward, S.H., Moller, J.C., Seymour, P.J.: Heat-flux measurements for the rotor of a full-stage turbine: Part II-description of analysis technique and typical time-resolved measurements. Trans. ASME J. Turbomach. 108(1), 98–107 (1986)CrossRef Dunn, M.G., Geroge, W.K., Rae, W.J., Woodward, S.H., Moller, J.C., Seymour, P.J.: Heat-flux measurements for the rotor of a full-stage turbine: Part II-description of analysis technique and typical time-resolved measurements. Trans. ASME J. Turbomach. 108(1), 98–107 (1986)CrossRef
6.
go back to reference George, W.K., Rae, W.J., Woodward, S.H.: An evaluation of analogue and numerical techniques for unsteady heat transfer measurements with thin-film gauges in transient facilities. Exp. Therm. Fluid Sci. 4(3), 333–342 (1991)CrossRef George, W.K., Rae, W.J., Woodward, S.H.: An evaluation of analogue and numerical techniques for unsteady heat transfer measurements with thin-film gauges in transient facilities. Exp. Therm. Fluid Sci. 4(3), 333–342 (1991)CrossRef
7.
go back to reference Hannemann, K., Martinez Schramm, J., Karl, S.: Recent extensions to the high enthalpy shock tunnel Göttingen (HEG). In 2nd International ARA Days (2008) Hannemann, K., Martinez Schramm, J., Karl, S.: Recent extensions to the high enthalpy shock tunnel Göttingen (HEG). In 2nd International ARA Days (2008)
8.
go back to reference Hubner, J.P., Carroll, B.F., Schanze, K.S., Ji, H.F. Holden, M.S.: Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow. AIAA Paper 99-0388 (1999) Hubner, J.P., Carroll, B.F., Schanze, K.S., Ji, H.F. Holden, M.S.: Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow. AIAA Paper 99-0388 (1999)
9.
go back to reference Hubner, J.P., Carroll, B.F., Schanze, K.S.: Heat Transfer Meas-urements in Hypersonic Flow Using Luminescent Coating Techniques. AIAA paper 2002-0741 (2002) Hubner, J.P., Carroll, B.F., Schanze, K.S.: Heat Transfer Meas-urements in Hypersonic Flow Using Luminescent Coating Techniques. AIAA paper 2002-0741 (2002)
10.
go back to reference Jessen, C.: Messung von Druck, Temperatur und Kraft an Modell im Stosswellenkanal, Dissertation RWTH Aachen (1993) Jessen, C.: Messung von Druck, Temperatur und Kraft an Modell im Stosswellenkanal, Dissertation RWTH Aachen (1993)
11.
go back to reference Kurits, I., Lewis, M.J.: Global temperature-sensitive paint system for heat transfer measurements in long-duration hypersonic flows. J. Thermophys. Heat Tran. 23(2), 256–266 (2009)CrossRef Kurits, I., Lewis, M.J.: Global temperature-sensitive paint system for heat transfer measurements in long-duration hypersonic flows. J. Thermophys. Heat Tran. 23(2), 256–266 (2009)CrossRef
12.
go back to reference Liu, T., Campbell, B.T., Sullivan, J.P.: Accuracy of Tempera-ture-Sensitive Fluorescent Paint for Heat Transfer Measure-ments. AIAA Paper 95-2042 (1995) Liu, T., Campbell, B.T., Sullivan, J.P.: Accuracy of Tempera-ture-Sensitive Fluorescent Paint for Heat Transfer Measure-ments. AIAA Paper 95-2042 (1995)
13.
go back to reference Liu, T., Sullivan, J.P.: Pressure and Temperature Sensitive Paints, p. 1. Springer, New York, chap (2005) Liu, T., Sullivan, J.P.: Pressure and Temperature Sensitive Paints, p. 1. Springer, New York, chap (2005)
14.
go back to reference Miller, C.G.: Comparison of Thin-Film Resistance Heat-Transfer Gages with Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels. NASA TM 83197 (1981) Miller, C.G.: Comparison of Thin-Film Resistance Heat-Transfer Gages with Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels. NASA TM 83197 (1981)
15.
go back to reference Martinez, S.J., Hannemann, K., Ozawa, H., Beck, W., Klein, C.: Development of Temperature Sensitive Paints for the High Enthalpy Shock Tunnel Göttingen, HEG. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon, Portugal (2015) Martinez, S.J., Hannemann, K., Ozawa, H., Beck, W., Klein, C.: Development of Temperature Sensitive Paints for the High Enthalpy Shock Tunnel Göttingen, HEG. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon, Portugal (2015)
16.
go back to reference Nagai, H., Ohmi, S., Asai, K.: Effect of temperature-sensitive-paint thickness on global heat transfer measurements in hypersonic flow. J. Thermophys. Heat Trans. 22(3), 373–381 (2008)CrossRef Nagai, H., Ohmi, S., Asai, K.: Effect of temperature-sensitive-paint thickness on global heat transfer measurements in hypersonic flow. J. Thermophys. Heat Trans. 22(3), 373–381 (2008)CrossRef
17.
go back to reference Nakakita, K., Osafune, T., Asai, K.: Global Heat Transfer Measurements in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint. AIAA Paper 2003-0743 (2003) Nakakita, K., Osafune, T., Asai, K.: Global Heat Transfer Measurements in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint. AIAA Paper 2003-0743 (2003)
19.
go back to reference Schultz, D.L., Jones, T.V.: Heat transfer measurements in short-duration hypersonic facilities. AGARD-AG-165 (1973) Schultz, D.L., Jones, T.V.: Heat transfer measurements in short-duration hypersonic facilities. AGARD-AG-165 (1973)
Metadata
Title
Calibration of Fast-Response Temperature Sensitive Paints for Their Application in Hypersonic High Enthalpy Flows
Authors
Jan Martinez Schramm
Frank Edzards
Klaus Hannemann
Copyright Year
2018
DOI
https://doi.org/10.1007/978-3-319-64519-3_13

Premium Partners