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12. Der Fan

verfasst von : Franz Joos

Erschienen in: Aerodynamik axialer Turbokompressoren

Verlag: Springer Fachmedien Wiesbaden

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Zusammenfassung

Um die gesteckten Ziele eines umweltfreundlichen Flugtriebwerkes, einen möglichst hohen Vortriebswirkungsgrad bei möglichst niedriger Lärmemission zu erreichen, werden immer höhere Bypassverhältnisse realisiert. Dieser Trend wird auch in naher Zukunft anhalten, um die politischen Vorgaben zu erfüllen. So strebt die EU-Kommission „European Aeronautics: Visio 2020“ in Kooperation mit dem „Advisory Council for Aeronautics Research in Europe" (ACARE) eine Halbierung der Lärm- und CO₂-Emission, sowie eine Absenkung der NOx-Werte um 80 % an.

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Vorheriges Kapitel Einfluss von Wassertropfen oder Partikeln in der Verdichterluft

Nächstes Kapitel Verdichterlärm

Podboy GG, Sutliff DL, Krupar MJ, Horvath C (2007) Shock charakteristics measured upstream of both a forward-swept and aft-swept Fan. In: Proceedings of ASME Turbo Expo 2007: power for land, sea, and air, Bd 6: Turbo Expo 2007, parts A and B, paper GT2007-27338, Montreal, Kanada, 14.–17. Mai 2007

Bräunling WJG (2015) Flugzeugtriebwerke, 4. Aufl. Springer Vieweg, Berlin/HeidelbergCrossRef

Grieb H (2009) Verdichter für Turboflugtriebwerke. Springer, Berlin/Heidelberg/New York

Calvert WJ, Ginder RB (1999) Transonic fan and compressor design. Proc Inst Mech Eng C J Mech Eng Sci 213(5):419–436

Denton JD, Xu L (2002) The effects of lean and sweep on transonic fan performance. In: Proceedings of ASME Turbo Expo 2002: power for land, sea, and air, Bd 5: Turbo Expo 2002, parts A and B, paper GT2002-30327, Amsterdam, Niederlande, 3.–6. Juni 2002

Neubert RJ, Hobbs DE, Weingold HD (1990) Application of sweep to improve the efficiency of a transonic fan. In: Proceedings Pts 1 & 2. AIAA 26th joint propulsion conference. Orlando, Juli 1990

Wadia AR, Szucs PNB, Crall DW (1997) Inner workings of aerodynamic sweep. In: Proceedings of ASME 1997 international gas turbine and aeroengine congress and exhibition, Bd 1: aircraft engine; marine; turbomachinery; microturbines and small turbomachinery, paper 97-GT-401, Orlando, Florida, Vereinigte Staaten von Amerika, 2.–5. Juni 1997

Kim S, Pullan G, Hall CA, Grewe RP, Wilson MJ, Lane M, Gunn E (2018) Stall inception in low pressure ratio fan. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-75153, Oslo, Norwegen, 11.–15. Juni 2018

Wadia AR, Niedermeier JD, Szucs PN, Cormier NG, Crall DW, Rabe DC (2018) Aerodynamic design and testing of an imbedded forward swept rotor in a two-stage transonic fan. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-75562, Oslo, Norwegen, 11.–15. Juni 2018

10.

John A, Qin N, Shahpar S (2018) Using shock control bumps to improve transonic fan/compressor blade performance. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-77065, Oslo, Norwegen, 11.–15. Juni 2018

11.

Wadia AR, Szucs PN, Crall DW, Rabe DC (2002) Forward swept rotor studies in multistage fans with inlet distortion. In: Proceedings of ASME Turbo Expo 2002: power for land, sea, and air, Bd 5: Turbo Expo 2002, parts A and B, paper GT2002-30326, Amsterdam, Niederlande, 3.–6. Juni 2002

12.

Wadia AR, James FD (2000) F110-GE-129 EFE – enhanced power through low risk derivative technology. In: ASME Turbo Expo 2000: power for land, sea, and air, Bd 1: aircraft engine; marine; turbomachinery; microturbines and small turbomachinery, paper 2000-GT-0578, München, Deutschland, 8.–11. Mai 2000

13.

Kaplan B, Nicke E, Voss C (2006) Design of a highly efficient low-noise fan for ultra-high bypass Engines. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2006-90363, Barcelona, Spanien, 8.–11. Mai 2006

14.

Denton JD (1993) Loss mechanisms in turbomachines. In Proceedings of ASME 1993 international gas turbine and aeroengine congress and exposition, Bd 2: combustion and fuels; oil and gas applications; cycle innovations; heat transfer; electric power; industrial and cogeneration; ceramics; structures and dynamics; controls, diagnostics and instrumentation; IGTI Scholar Award, Cincinnati, Ohio, Vereinigte Staaten von Amerika, 24.–27. Mai 1993

15.

Storer J, Cumpsty N (1994) An approximate analysis and prediction method for tip clearance loss in axial compressors. ASME J Turbomach 116(4):648–656CrossRef

16.

Sieverding C (1985) Tip clearance effects in axial Turbomachines, April 15–19, 1985. Von Karman Institute for Fluid Dynamics

17.

Kammer AS, Olgac N (2016) Blade/casing rub interaction in turbomachinery: structural parameters influence on stability. J Propulsion Power 32(1):1–10CrossRef

18.

Ma H, Yin F, Guo Y, Tai X, Wen B (2016) A review on dynamic characteristics of blade–casing rubbing. Nonlinear Dynam 84(2):437–472CrossRef

19.

Fois N, Watson M, Marshall M (2016) The influence of material properties on the wear of abradable materials. Proc Inst Mech Eng J J Eng Tribol 231(2):240–253CrossRef

20.

Legrand M, Batailly A, Pierre C (2012) Numerical investigation of abradable coating removal in aircraft engines through plastic constitutive law. ASME J Comput Nonlinear Dynam 7(1):11

21.

John A, Qin N, Shahpar S (2017) Fan blade tip aerodynamik with realistic operational casing geometries and clearances. In: Proceedings of ASME Turbo Expo 2017: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2017-64403, Charlotte, North Carolina, Vereinigte Staaten von Amerika, 26.–30. Juni 2017

22.

Adamczyk J, Celestina M, Greitzer E (1991) The role of tip clearance in high-speed fan stall. In: Proceedings of ASME 1991 international gas turbine and aeroengine congress and exposition, Bd 1: turbomachinery, paper 91-GT-083, Orlando, Florida, Vereinigte Staaten von Amerika, 3.–6. Juni 1991

23.

Sakulkaew S, Tan C, Donahoo E, Cornelius C, Montgomery M (2013) Compressor efficiency variation with rotor tip gap from vanishing to large clearance. ASME J Turbomach 135(3):10

24.

Seshadri P, Shahpar S, Parks GT (2014) Robust compressor blades for desensitizing operational tip clearance variations. In: Proceedings of ASME Turbo Expo 2014: turbine technical conference and exposition, Bd 2A: turbomachinery, paper GT2014-26624, Düsseldorf, Deutschland, 16.–20. Juni 2014

25.

Shabbir A, Adamczyk JJ (2005) Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors. ASME J Turbomach 127(4):708–717CrossRef

26.

Houghton T, Day I (2012) Stability enhancement by casing grooves: the importance of stall inception mechanism and solidity. ASME J Turbomach 134(2):8

27.

Qin N, Carnie G, Wang Y, Shahpar S (2014) Design optimization of casing grooves using zipper layer meshing. ASME J Turbomach 136(3):031002CrossRef

28.

Robideau BA, Niiler J (1980) Blade tip seal for an axial flow rotary machine, December 9. US Patent 4,238,170

29.

Korting P, Beacher B (1989) Improved compressor performance using recessed clearance (trenches). J Propulsion Power 5(4):469–475CrossRef

30.

Esgar GM, Sandercock DM (1973) Some observed effects of part span dampers on rotating blade row performance near design point. NASA-TM X-2696

31.

Benser WA, Bailey EE, Gelder TF (1975) Holographic studies of shock waves within transonic fan rotors. ASME Trans J Eng Power 97:75–84CrossRef

32.

Reid L, Tysl ER (1974) Performance of a transonic rotor with an aspect ratio of 6.5. NASA TN D-7662

33.

Lewis GW, Urasek DC (1972) Comparison of the effect of two damper sizes on the performance of a low solidity axial flow transonic compressor rotor. NASA TMX-2536

34.

Messenger HE, Keenan MJ (1974) Two stage fan 2: data and performance with redesigned second stage rotor uniform and distorted inlet flows. NASA CR-134710

35.

Ware TC, Kobayashi RJ, Jackson RJ (1974) High tip speed low loading transonic fan stage. Part 3: final report, NASA CR-121263

36.

Koch CC, Smith LH Jr (1975) Loss sources and magnitudes in axial-flow compressors. ASME paper no. 75-WA/GT-6

37.

Roberts WB (1978) A design point correlation for losses due to part span dampers on transonic rotors. ASME paper no. 78-GT-153

38.

Wadia AR, Szucs PN (2006) Inner workings of shrouded and un-shrouded transonic fan blades. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2006-90992, Barcelona, Spanien, 8.–11. Mai 2006

39.

Longley JP, Greitzer EM (1992) Inlet distortion effects in aircraft propulsion system integration. In: Steady and transient performance prediction of gas turbine engines, Vol. 183 of AGARD Lecture Series. Chapter 7

40.

Mehalic C (1988) Effect of spatial inlet temperature and pressure distortion on turbofan engine stability. NASA-TM-100850 (AIAA-88-3016)

41.

Jiang H, Lu Y, Yuan W, Li Q (2009) Experimental investigation of the influence of inlet distortion on the stall inception in a low speed axial compressor. In: Proceedings of ASME Turbo Expo 2009: power for land, sea, and air, Bd 7: turbomachinery, parts A and B, paper GT2009-59139, Orlando, Florida, Vereinigte Staaten von Amerika, 8.–12. Juni 2009

42.

Gunn E, Tooze S, Hall C, Colin Y (2012) An experimental study of loss sources in a fan operating with continuous inlet stagnation pressure distortion. In: Proceedings of ASME Turbo Expo 2012: turbine technical conference and exposition, Bd 8: turbomachinery, parts A, B, and C, paper GT2012-68888, Kopenhagen, Dänemark, 11.–15. Juni 2012

43.

Connell S, Braaten M, Zori L, Steed R, Hutchinson B, Cox G (2011) A comparison of advanced numerical techniques to model transient flow in turbomachinery blade rows. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45820, Vancouver, Kanada, 6.–10. Juni 2011

44.

Giles M (1988) Calculation of unsteady wake/rotor interaction. J Propulsion Power 4(4):356–362CrossRef

45.

Biesinger T, Cornelius C, Rube C, Schmid G, Braune A, Campregher C, Godin P, Zori L (2010) Unsteady CFD methods in a commercial solver for turbomachinery applications. In: Proceedings of ASME Turbo Expo 2010: power for land, sea, and air, Bd 7: turbomachinery, parts A, B, and C, paper GT2010-22762, Glasgow, Großbritannien, 14.–18. Juni 2010

46.

He L (1990) An Euler solution for unsteady flows around oscillating blades. ASME J Turbomach 112(4):714–722CrossRef

47.

Gerolymos G, Michon G, Neubauer J (2002) Analysis and application of chorochronic periodicity in turbomachinery rotor/stator interaction computations. J Propulsion Power 9(6):1139–1152CrossRef

48.

Brailko I, Mileshin V, Volkov A, Korznev V (2010) Numerical and experimental investigations of CRF with simulation of flow non-uniformity in the basic flight conditions. In: Proceedings of 27th congress of international council of the aeronautical sciences, ICAS 2010-4.2.2, Nizza, Frankreich, 2010

49.

Lesser A, Iseler J, Niehuis R (2011) Numerical investigation of a highly loaded axial compressor stage with inlet distortions. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45457, Vancouver, Kanada, 6.–10. Juni 2011

50.

Fidalgo V, Hall C, Colin Y (2010) A study of fan- distortion interaction within the NASA Rotor 67 transonic stage. In: Proceedings of ASME Turbo Expo 2010: power for land, sea, and air, Bd 7: turbomachinery, parts A, B, and C, paper GT2010-22914, Glasgow, Großbritannien, 14.–18. Juni 2010

51.

Herrick G (2011) Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan. NASA TM-2011-216959 (AIAA-2010-6711)

52.

Yao J, Gorrell S, Wadia A (2008a) High-fidelity numerical analysis of per-rev-type inlet distortion transfer in multistage fans – Part I: simulations with selected blade rows. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 6: turbomachinery, parts A, B, and C, paper GT2008-50812, Berlin, Deutschland, 9.–13. Juni 2008

53.

Sharma G, Zori L, Connel S, Godin P (2013) Efficient computation of large pitch ratio transonic flow in a fan with inlet distortion. In: Proceedings of ASME Turbo Expo 2013: turbine technical conference and exposition, Bd 6C: turbomachinery, paper GT2013-95059, San Antonio, Texas, Vereinigte Staaten von Amerika, 3.–7. Juni 2013

54.

Florea RV, Matalanis C, Hardin LW, Stucky M, Shabbir A (2015) Parametric analysis and design for embedded engine inlets. J Propulsion Power 31(3):851–860

55.

Fidalgo VJHCA, Colin Y (2012) A study of fan-distortion interaction within the NASA rotor 67 transonic stage. ASME Turbomach 134(5):051011CrossRef

56.

Gunn EJ, Tooze SE, Hall CA, Colin Y (2013) An experimental study of loss sources in a fan operating with continuous inlet stagnation pressure distortion. ASME J Turbomach 135(5):051002–051002–10. https://doi.org/10.1115/1.4007835CrossRef

57.

Gunn EJ, Hall CA (2014) Aerodynamics of boundary layer ingesting fans. In: Proceedings of ASME Turbo Expo 2014: turbine technical conference and exposition. Proceedings of ASME Turbo Expo 2014: turbine technical conference and exposition, Bd 1A: aircraft engine; fans and blowers, paper GT2014-26142, Düsseldorf, Deutschland, 16.–20. Juni 2014

58.

Madani V, Hynes T (2009) Boundary layer ingesting intakes: design and optimization. In: Presented at the 19th ISABE conference, ISABE paper 2009-1346, 7.–11. Sept. 2009, Montreal, Canada

59.

Perovic D, Hall CA, Gunn EJ (2015) Stall inception in a boundary layer ingesting fan. In: Proceedings of ASME Turbo Expo 2015: turbine technical conference and exposition. Proceedings of ASME Turbo Expo 2015: turbine technical conference and exposition, Bd 2A: turbomachinery, paper GT2015-43025, Montreal, Quebec, Kanada, 15.–19. Juni 2015

60.

Hall DK (2015) Analysis of civil aircraft propulsors with boundary layer ingestion. PhD thesis, Massachusetts Institute of Technology

61.

Hall DK, Greitzer EM, Tan CS (2016) Analysis of fan stage design attributes for boundary layer ingesting propulsion. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-57808, Seoul, Südkorea, 13.–17. Juni 2016

62.

Marble F (1964) Three-dimensional flow in turbomachines. High Speed Aerodynam Jet Propulsion 10:83–166

63.

Horlock J (1971) On entropy production in adiabatic flow in turbomachines. ASME J Fluids Eng 93(4):587–593

64.

Horlock J, Marsh H (1971) Flow models for turbomachines. J Mechan Eng Sci 13(5):358–368CrossRef

65.

Gong Y, Tan C, Gordon K, Greitzer E (1999) A computational model for short-wavelength stall inception and development in multi-stage compressors. ASME J Turbomach 121(4):726–734CrossRef

66.

Peters A, Spakovszky ZS, Lord WK, Rose B (2015) Ultrashort nacelles for low fan pressure ratio propulsors. ASME J Turbomach 137(2):021001CrossRef

67.

Defoe JJ, Spakovszky ZS (2013) Effects of boundary-layer ingestion on the aero-acoustics of transonic fan rotors. ASME J Turbomach 135(5):051013CrossRef

68.

Defoe JJ, Hall DK (2016) Fan performance scaling with inlet distortions. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-58009, Seoul, Südkorea, 13.–17. Juni 2016

69.

Guillard V (2014) Study of the fan forced response due to crosswind. University essay from KTH/Aerodynamik

70.

Lobo B, Zori L, Galpin P (2016) Efficient modeling strategy of an axial compressor fan-stage under inlet distortion. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-57467, Seoul, Südkorea, 13.–17. Juni 2016

71.

Ferrar AM, Schneck III W, Wicks A, O’Brien W (2016) Effects of total pressure inlet distortion on transonic fannn blade wake properties. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-57703, Seoul, Südkorea, 13–17 Juni 2016

72.

Ferrar AM (2015) Measurement and uncertainty analysis of transonic fan response to total pressure inlet distortion. PhD thesis, Virginia Polytechnic Institute and State University

73.

Pankov SV, Mileshin VI, Orekhov IK, Fateev VA (2017) Development of direct-driven and geared fan stages with reduced speed. In: Proceedings of ASME Turbo Expo 2017: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2006-90582, Charlotte, North Carolina, Vereinigte Staaten von Amerika, 26.–30. Juni 2017

74.

Kerrebrook JL, Epstein AH, Merchant AA, Guenette GR, Parker D, Onnee J-F, Neumayer F, Adamcyk JJ, Shabbir A (2006) Design and test of an aspirated counter-rotating fan. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2006-90582, Barcelona, Spanien, 8.–11. Mai 2006

75.

Sullivan TJ (1990) Aerodynamic performance of a scale-model, counterrotating unducted fan. ASME J Turbomach 112(4):579–586CrossRef

76.

Smith LH Jr (1987) Unducted fan aerodynamic design. ASME J Turbomach 109(3):313–324CrossRef

77.

Hager RD, Vrabel D (1988) Advanced turboprop project. NASA SP-495

78.

Mitchell GA (1988) Experimental aerodynamic performance of advanced 40-Swept, 10-Blade Propeller Model at Mach 0.6 to 0.85, NASA TM-88969

79.

Neumann HE, Bober LJ, Serafini JS, Chang L-K (1983) An analytical and experimental comparison of the flow field of an advanced swept turboprop. In: Proceedings of 21st aerospace sciences meeting, paper AIAA-1983-189, Reno, Nevada, Vereinigte Staaten von Amerika, 10.–13. Januar 1983

80.

Podboy GG, Krupar MJ (1989) Laser velocimeter measurements of the flow field generated by an advanced counterrotating propeller. In: Proceedings of 27th aerospace sciences meeting, paper AIAA-1989-434, Reno, Nevada, Vereinigte Staaten von Amerika, 9.–12. Januar 1989

81.

Shin H-W, Whitfield CE, Wisler DC (1994) Rotor-rotor interaction for counter-rotating fans, part 1: three-dimensional flowfield measurements. AIAA J 32(11):2224–2233CrossRef

82.

Celestina ML, Mulac RA, Adamczyk JJ (1986) A numerical simulation of the inviscid flow through a counter-rotating propeller. ASME J Turbomach 108(2):187–193CrossRef

83.

Zachariadis A, Hall CA (2009) Application of a navier-stokes solver to the study of open rotor aerodynamics. In: ASME Proceedings of ASME Turbo Expo 2009: power for land, sea, and air, Bd 7: turbomachinery, parts A and B, paper GT2009-59332, Orlando, Florida, Vereinigte Staaten von Amerika, 8.–12. Juni 2009

84.

Schnell R, Yin Y, Voss C, Nicke E (2010) Assessment and optimization of the aerodynamic and acoustic characteristics of a counter rotating open rotor. In: Proceedings of ASME Turbo Expo 2010: power for land, sea, and air, Bd 7: turbomachinery, parts A, B, and C, paper GT2010-22076, Glasgow, Großbritannien, 14.–18. Juni 2010

85.

Peters A, Spakovszky ZS (2010) Rotor interaction noise in counter-rotating propfan propulsion systems. In: Proceedings of ASME Turbo Expo 2010: power for land, sea, and air, Bd 7: turbomachinery, parts A, B, and C, GT2010-22554, Glasgow, Großbritannien, 14.–18. Juni 2010

86.

Zachariadis A, Hall CA, Parry AB (2011) Contra-rotating open rotor operation for improved aerodynamics and noise at take off. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45205, Vancouver, Kanada, 6.–10. Juni 2011

87.

Kirker TJ (1990) Procurement and testing of a 1/5 scale advanced counter rotating propfan model. In: Proceedings of 13th aeroacoustics conference, paper AIAA-1990-3975, Tallahassee, Florida, Vereinigte Staaten von Amerika, 22.–24. Oktober 1990

88.

Moinier P, Giles MB (1998) Preconditioned Euler and navier-stokes calculations on unstructured grids. In 6th ICFD conference on numerical methods for fluid dynamics, Oxford, Großbritannien, 1998

89.

Whitfield CE, Mani R, Gliebe PR (1990a) High speed turboprop acoustic study (counterrotation), Bd II, computer programs. Technical report, NASA CR-185242

90.

Whitfield CE, Mani R, Gliebe PR (1990b) High speed turboprop acoustic study (counterrotation), Bd I, model development. Technical report, NASA CR-185241

91.

Khalid SA, Wojno JP, Breeze-Stringfellow A, Lurie DP, Wood TH, Ramakrishnan K, Paliath U (2013) Open rotor designs for low noise high efficiency. In: Proceedings of ASME Turbo Expo 2013: turbine technical conference and exposition, Bd 6C: turbomachinery, paper GT2013-94736, San Antonio, Texas, Vereinigte Staaten von Amerika, 3.–7. Juni 2013

92.

Van Zante DE (2015) Progress in open rotor research: a US perspective. In: Proceedings of ASME Turbo Expo 2015: turbine technical conference and exposition, Bd 1: aircraft engine; fans and blowers; marine, paper GT2015-42203, Montreal, Quebec, Kanada, 15.–19. Juni 2015

93.

ICAO (2013) Final report, noise technology Independent Expert Panel (IEP2), ICAO CAEP/9-WP16

94.

EASA (2011) Open rotor engine & installation, terms of reference. EASA-ToR-MDM.092

95.

Courty-Audren S-K (2015) Identification et compréhension des mecanismes aerodynamiques lies au potentiel de recuperation d’energie. Application a un ventilateur axial subsonique en autorotation. PhD thesis, ISAE-SUPAERO

96.

Gunn EJ, Hall CA (2015) Loss and deviation in windmilling fans. In: Proceedings of the 11th European conference on turbomachinery, paper ETC2015-061, Madrid, Spanien, 23.–27. März 2015

97.

Garcia Rosa N, Pilet J, Lecordix J-L, Barenes R, Lavergne G (2013) Experimental analysis of the flow through the fan stage of a high-bypass turbofan in windmilling conditions. In: Proceedings of the 10th European conference on turbomachinery, paper ETC2013-162, Lappeenranta, Finnland, 15.–19. April 2013

98.

Prasad D, Lord WK (2010) Internal losses and flow behavior of a turbofan stage at windmill. ASME J Turbomach 132(3):031007–10CrossRef

99.

Binder N, Courty-Audren S-K, Duplaa S, Dufour G, Carbonneau X (2015) Theoretical analysis of the aerodynamics of low-speed fans in free and load controlled windmilling operation. ASME J Turbomach 137(10):101001–101012CrossRef

100.

Gill A (2011) Four quadrant axial flow compressor performance. PhD thesis, Stellenbosch University

101.

Ortolan A, Courty-Audren S-K, Challas F (2016) Experimental and numerical flow analysis of low-speed fans at highly loaded windmilling conditions. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-56577, Seoul, Südkorea, 13.–17. Juni 2016

102.

Ortolan A, Carbonneau X, Binder N, Challas F, Meauze G (2015) Innovative fan design for both high compressor and windmilling performance. In: Proceedings of the 12th international symposium on experimental and computational aerothermodynamics of internal flows, paper ISAIF12-068, Lerici, Italien, 13.–16. Juli 2015

103.

Prasad D, Lord WK (2010) Internal losses and flow behavior of a turbofan stage at windmill. ASME J Turbomach 132(3):031007CrossRef

104.

Prasad D (2018) Aerodynamic similarity principles and scaling laws for windmilling fans. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-76640, Oslo, Norwegen, 11.–15. Juni 2018

Titel: Der Fan
verfasst von: Franz Joos
Verlag: Springer Fachmedien Wiesbaden
Buch: Aerodynamik axialer Turbokompressoren
Print ISBN: 978-3-658-28936-2

Electronic ISBN: 978-3-658-28937-9

Copyright-Jahr: 2020
DOI: https://doi.org/10.1007/978-3-658-28937-9_12

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