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2020 | OriginalPaper | Buchkapitel

2. Grundlagen der Aerodynamik

verfasst von : Franz Joos

Erschienen in: Aerodynamik axialer Turbokompressoren

Verlag: Springer Fachmedien Wiesbaden

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Zusammenfassung

Zur Berechnung der Hauptbetriebsdaten der Strömungsmaschinen werden die aus der Strömungsmechanik bekannten Bilanzen

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Literatur
1.
Zurück zum Zitat Traupel W (1988) Thermische Turbomaschinen, Bd 1. Springer, Berlin/Heidelberg/New YorkMATH Traupel W (1988) Thermische Turbomaschinen, Bd 1. Springer, Berlin/Heidelberg/New YorkMATH
2.
Zurück zum Zitat Traupel W (1988) Thermische Turbomaschinen, Bd 2. Springer, Berlin/Heidelberg/New YorkMATH Traupel W (1988) Thermische Turbomaschinen, Bd 2. Springer, Berlin/Heidelberg/New YorkMATH
3.
Zurück zum Zitat Lechner G, Seume J (2003) Stationäre Gasturbinen. Springer, Berlin/Heidelberg/New YorkCrossRef Lechner G, Seume J (2003) Stationäre Gasturbinen. Springer, Berlin/Heidelberg/New YorkCrossRef
4.
Zurück zum Zitat Rick H (2013) Gasturbinen und Flugantriebe: Grundlagen, Betriebsverhalten und Simulation. Springer Vieweg, Berlin/HeidelbergCrossRef Rick H (2013) Gasturbinen und Flugantriebe: Grundlagen, Betriebsverhalten und Simulation. Springer Vieweg, Berlin/HeidelbergCrossRef
5.
Zurück zum Zitat Riegels FW (1958) Aerodynamische Profile. Verlag, OldenbourgMATH Riegels FW (1958) Aerodynamische Profile. Verlag, OldenbourgMATH
6.
Zurück zum Zitat Bohl W, Elemendorf W (2012) Strömungsmaschinen 1: Aufbau und Wirkungsweise, Kamprath-Reihe, 11. Aufl. Vogel Communications Group GmbH & Co. KG, Würzburg Bohl W, Elemendorf W (2012) Strömungsmaschinen 1: Aufbau und Wirkungsweise, Kamprath-Reihe, 11. Aufl. Vogel Communications Group GmbH & Co. KG, Würzburg
7.
Zurück zum Zitat Grieb H (2009) Verdichter für Turbo-Flugtriebwerke. Springer-Verlag, Berlin Grieb H (2009) Verdichter für Turbo-Flugtriebwerke. Springer-Verlag, Berlin
8.
Zurück zum Zitat Emery JC, Herrig LJ, Erwin JR, Felix AR (1958) Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds. NACA report 1368, NACA Washington, DC Emery JC, Herrig LJ, Erwin JR, Felix AR (1958) Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds. NACA report 1368, NACA Washington, DC
9.
Zurück zum Zitat Kovach K, Sanderock DM (1961) Aerodynamic design and performance of five stage transonic axial flow compressor. ASME J Eng Pow 83:304–321 Kovach K, Sanderock DM (1961) Aerodynamic design and performance of five stage transonic axial flow compressor. ASME J Eng Pow 83:304–321
10.
Zurück zum Zitat Cumpsty NA (1989) Compressor aerodynamics. Longman Scientific and Technical, Essex Cumpsty NA (1989) Compressor aerodynamics. Longman Scientific and Technical, Essex
11.
12.
Zurück zum Zitat Behlke RF (1986) The development of a second generation of controlled diffusion airfoils for multistage compressors. ASME J Turbomach 108(1):32–41CrossRef Behlke RF (1986) The development of a second generation of controlled diffusion airfoils for multistage compressors. ASME J Turbomach 108(1):32–41CrossRef
13.
Zurück zum Zitat Hobbs DE, Weingold HD (1984) Development of controlled diffusion airfoils for multistage compressor application. ASME J Eng Gas Turbines Power 106(2):271–278CrossRef Hobbs DE, Weingold HD (1984) Development of controlled diffusion airfoils for multistage compressor application. ASME J Eng Gas Turbines Power 106(2):271–278CrossRef
14.
Zurück zum Zitat Voss C, Aulich M, Kaplan B, Nicke E (2006) Automated multi-objective optimisation in axial compressor blade design. In: Proceedings of ASME Turbo Expo 2006: power for land, sea and air, volume 6: turbomachinery, parts A and B. Paper GT2006-0420, Barcelona, Spain, 8–11 May Voss C, Aulich M, Kaplan B, Nicke E (2006) Automated multi-objective optimisation in axial compressor blade design. In: Proceedings of ASME Turbo Expo 2006: power for land, sea and air, volume 6: turbomachinery, parts A and B. Paper GT2006-0420, Barcelona, Spain, 8–11 May
15.
Zurück zum Zitat Bitterlich W, Ausmeier S (2002) Gasturbinen und Gasturbinenanlagen: Darstellung und Berechnung. Vieweg Teubner, WiesbadenCrossRef Bitterlich W, Ausmeier S (2002) Gasturbinen und Gasturbinenanlagen: Darstellung und Berechnung. Vieweg Teubner, WiesbadenCrossRef
16.
Zurück zum Zitat Hergt A, Klinner J, Wellner J, Willert C, Grund S, Steinert W, Beversdorff M (2018) The present challenge of transonic compressor blade design. In: Proceedings of ASME Turbo Expo 2018. Turbomachinery technical conference and exposition, paper GT2018-75528, Oslo, Norway, 11–15 June Hergt A, Klinner J, Wellner J, Willert C, Grund S, Steinert W, Beversdorff M (2018) The present challenge of transonic compressor blade design. In: Proceedings of ASME Turbo Expo 2018. Turbomachinery technical conference and exposition, paper GT2018-75528, Oslo, Norway, 11–15 June
17.
Zurück zum Zitat Denton JD (1993) The 1993 IGTI scholar lecture: loss mechanisms in turbomachines. ASME J Turbomach 115(4):621CrossRef Denton JD (1993) The 1993 IGTI scholar lecture: loss mechanisms in turbomachines. ASME J Turbomach 115(4):621CrossRef
18.
Zurück zum Zitat Williams R, Gregory-Smith D, He L, Ingram G (2010) Experiments and computations on large tip clearance effects in a linear cascade. ASME J Turbomach 132(2):021018CrossRef Williams R, Gregory-Smith D, He L, Ingram G (2010) Experiments and computations on large tip clearance effects in a linear cascade. ASME J Turbomach 132(2):021018CrossRef
19.
Zurück zum Zitat Storer JA, Cumpsty NA (1991) Tip leakage flow in axial compressors. ASME J Turbomach 113(2):252–259CrossRef Storer JA, Cumpsty NA (1991) Tip leakage flow in axial compressors. ASME J Turbomach 113(2):252–259CrossRef
20.
Zurück zum Zitat Yoon YS, Song SJ, Shin H-W (2006) Influence of flow coefficient, stagger angle, and tip clearance on tip vortex in axial compressors. ASME J Fluids Eng 128(6):1274–1280CrossRef Yoon YS, Song SJ, Shin H-W (2006) Influence of flow coefficient, stagger angle, and tip clearance on tip vortex in axial compressors. ASME J Fluids Eng 128(6):1274–1280CrossRef
21.
Zurück zum Zitat Bae J, Breuer KS, Tan CS (2004) Periodic unsteadiness of compressor tip clearance vortex. In: Proceedings ASME Turbo Expo 2004: power for land, sea and air, volume 6: Turbo Expo 2004, paper GT2004-53015,Vienna, Austria, 14–17 June, S 457–465 Bae J, Breuer KS, Tan CS (2004) Periodic unsteadiness of compressor tip clearance vortex. In: Proceedings ASME Turbo Expo 2004: power for land, sea and air, volume 6: Turbo Expo 2004, paper GT2004-53015,Vienna, Austria, 14–17 June, S 457–465
22.
Zurück zum Zitat Hwang Y, Kang S-H, Lee S (2010) Numerical study on unsteadiness of tip clearance flow induced by downstream stator row in axial compressor. In: Proceedings of ASME Turbo Expo 2010: power for land, sea and air, volume7: turbomachinery, parts A, B, and C, paper GT2010-23024, Glasgow, UK, 14–18 June, S 2553–2560 Hwang Y, Kang S-H, Lee S (2010) Numerical study on unsteadiness of tip clearance flow induced by downstream stator row in axial compressor. In: Proceedings of ASME Turbo Expo 2010: power for land, sea and air, volume7: turbomachinery, parts A, B, and C, paper GT2010-23024, Glasgow, UK, 14–18 June, S 2553–2560
23.
Zurück zum Zitat Smith LH (1966) Wake dispersion in turbomachines. J Basic Eng 88(3):688CrossRef Smith LH (1966) Wake dispersion in turbomachines. J Basic Eng 88(3):688CrossRef
24.
Zurück zum Zitat Van Zante DE, Adamczyk JJ, Strazisar AJ, Okiishi TH (2002) Wake recovery performance benefit in a 12 Copyright © 2016 by Siemens Energy Inc., high-speed axial compressor. J Turbomach 124(2):275CrossRef Van Zante DE, Adamczyk JJ, Strazisar AJ, Okiishi TH (2002) Wake recovery performance benefit in a 12 Copyright © 2016 by Siemens Energy Inc., high-speed axial compressor. J Turbomach 124(2):275CrossRef
25.
Zurück zum Zitat Valkov TV, Tan CS (1999) Effect of upstream rotor vortical disturbances on the time-averaged performance of axial compressor stators: part 1: framework of technical approach and wake-stator blade interactions. J Turbomach 121(3):377CrossRef Valkov TV, Tan CS (1999) Effect of upstream rotor vortical disturbances on the time-averaged performance of axial compressor stators: part 1: framework of technical approach and wake-stator blade interactions. J Turbomach 121(3):377CrossRef
26.
Zurück zum Zitat Valkov TV, Tan CS (1999) Effect of upstreamrotor vortical disturbances on the time-averaged performance of axial compressor stators: part 2: rotor tip vortex/streamwise vortex-stator blade interactions. J Turbomach 121(3):387CrossRef Valkov TV, Tan CS (1999) Effect of upstreamrotor vortical disturbances on the time-averaged performance of axial compressor stators: part 2: rotor tip vortex/streamwise vortex-stator blade interactions. J Turbomach 121(3):387CrossRef
27.
Zurück zum Zitat Gallimore SJ, Bolger JJ, Cumpsty NA, Taylor MJ, Wright PI, Place JMM (2002) The use of sweep and dihedral in multistage axial flow compressor blading; part I: university research and methods development. J Turbomach 124(4):521CrossRef Gallimore SJ, Bolger JJ, Cumpsty NA, Taylor MJ, Wright PI, Place JMM (2002) The use of sweep and dihedral in multistage axial flow compressor blading; part I: university research and methods development. J Turbomach 124(4):521CrossRef
28.
Zurück zum Zitat Gallimore SJ, Bolger JJ, Cumpsty NA, Taylor MJ, Wright PI, Place JMM (2002) The use of sweep and dihedral in multistage axial flow compressor blading; part II: low and high-speed designs and test verification. J Turbomach 124(4):533CrossRef Gallimore SJ, Bolger JJ, Cumpsty NA, Taylor MJ, Wright PI, Place JMM (2002) The use of sweep and dihedral in multistage axial flow compressor blading; part II: low and high-speed designs and test verification. J Turbomach 124(4):533CrossRef
29.
Zurück zum Zitat Buche D, Guidati G, Stoll P (2003) Automated design optimization of compressor blades for stationary, large-scale turbomachinery. In: ASME Turbo Expo 2003, collocated with the 2003 international joint power generation conference volume 6: Turbo Expo 2003, parts A and B, paper GT2003-38421, Atlanta, Georgia, USA, 16–19 June, S 1249–1257 Buche D, Guidati G, Stoll P (2003) Automated design optimization of compressor blades for stationary, large-scale turbomachinery. In: ASME Turbo Expo 2003, collocated with the 2003 international joint power generation conference volume 6: Turbo Expo 2003, parts A and B, paper GT2003-38421, Atlanta, Georgia, USA, 16–19 June, S 1249–1257
30.
Zurück zum Zitat Seshadri P, Shahpar S, Parks GT (2014) Robust compressor blades for desensitizing operational tip clearance variations. In: ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2A: turbomachinery, paper GT2014-26624, Düsseldorf, Germany, 16–20 June, S V02AT37A043 Seshadri P, Shahpar S, Parks GT (2014) Robust compressor blades for desensitizing operational tip clearance variations. In: ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2A: turbomachinery, paper GT2014-26624, Düsseldorf, Germany, 16–20 June, S V02AT37A043
31.
Zurück zum Zitat Wisler DC (1985) Loss reduction in axial-flow compressors through low-speed model testing. J Eng Gas Turbines Power 107(2):354CrossRef Wisler DC (1985) Loss reduction in axial-flow compressors through low-speed model testing. J Eng Gas Turbines Power 107(2):354CrossRef
32.
Zurück zum Zitat Tiralap A, Tan CS, Donahoo E, Montgomery M, Cornelius C (2016) Effects of rotor tip blade loading variation on compressor stage performance. In: Proceedings ASME Turbo Expo 2016: turbomachinery technical conference and exposition, volume 2A: turbomachinery, paper GT2016-57727, Seoul S-Korea, 13–17 June Tiralap A, Tan CS, Donahoo E, Montgomery M, Cornelius C (2016) Effects of rotor tip blade loading variation on compressor stage performance. In: Proceedings ASME Turbo Expo 2016: turbomachinery technical conference and exposition, volume 2A: turbomachinery, paper GT2016-57727, Seoul S-Korea, 13–17 June
33.
Zurück zum Zitat Taghavi-Zenouz R, Eslami S (2011) Numerical simulation of unsteady tip clearance flow in an isolated axialcompressor rotor blades row. In: Proceedings of the Institution of Mechanical Engineers, part C: J Mech Eng Sci, 226(1):82–93 Taghavi-Zenouz R, Eslami S (2011) Numerical simulation of unsteady tip clearance flow in an isolated axialcompressor rotor blades row. In: Proceedings of the Institution of Mechanical Engineers, part C: J Mech Eng Sci, 226(1):82–93
34.
Zurück zum Zitat Zhang H, Deng X, Lin F, Chen J, Huang W (2006) A study on the mechanism of tip leakage flow unsteadiness in an isolated compressor rotor. In: Proceedings ASME Turbo Expo 2006: power for land, sea, and air, volume 6: turbomachinery, parts A and B, paper GT2006-91123, Barcelona, Spain, 8–11 May, S 435–445 Zhang H, Deng X, Lin F, Chen J, Huang W (2006) A study on the mechanism of tip leakage flow unsteadiness in an isolated compressor rotor. In: Proceedings ASME Turbo Expo 2006: power for land, sea, and air, volume 6: turbomachinery, parts A and B, paper GT2006-91123, Barcelona, Spain, 8–11 May, S 435–445
35.
Zurück zum Zitat Hergt A, Steinert W, Grund S (2013) Design and experimental investigation of a compressor cascade for low reynolds number conditions. In: ISABE paper, 21st ISABE conference Busan/Korea, September 2013 Hergt A, Steinert W, Grund S (2013) Design and experimental investigation of a compressor cascade for low reynolds number conditions. In: ISABE paper, 21st ISABE conference Busan/Korea, September 2013
36.
Zurück zum Zitat Denton JD (1993) The 1993 IGTI Scholar lecture: loss mechanisms in turbomachines. J Turbomach 115(4):621–656CrossRef Denton JD (1993) The 1993 IGTI Scholar lecture: loss mechanisms in turbomachines. J Turbomach 115(4):621–656CrossRef
37.
Zurück zum Zitat Van Zante DE, Adamczyk JJ, Strazisar AJ, Okiishi TH (2002) Wake recovery performance benefit in a high speed axial compressor. ASME J Turbomach 124:275–284CrossRef Van Zante DE, Adamczyk JJ, Strazisar AJ, Okiishi TH (2002) Wake recovery performance benefit in a high speed axial compressor. ASME J Turbomach 124:275–284CrossRef
38.
Zurück zum Zitat Adamczyk JJ (1996) Wake mixing in axial flow compressors. In: Proceedings ASME 1996 international gas turbine and aeroengine congress and exhibition, vol. 1: turbomachinery, paper 96-GT-029, Birmingham, UK, 10–13 June Adamczyk JJ (1996) Wake mixing in axial flow compressors. In: Proceedings ASME 1996 international gas turbine and aeroengine congress and exhibition, vol. 1: turbomachinery, paper 96-GT-029, Birmingham, UK, 10–13 June
39.
Zurück zum Zitat Zaki T, Wissink J, Durbin PA, Rodi W (2010) Direct numerical simulations of transition in a compressor cascade: the influence of free-stream turbulence. J Fluid Mech 665:57–98CrossRef Zaki T, Wissink J, Durbin PA, Rodi W (2010) Direct numerical simulations of transition in a compressor cascade: the influence of free-stream turbulence. J Fluid Mech 665:57–98CrossRef
40.
Zurück zum Zitat Hah C, Shin H (2012) Study of near –stall flow behavior in a modern transonic fan with compound sweep. ASME J Fluids Eng 134:071101–071107CrossRef Hah C, Shin H (2012) Study of near –stall flow behavior in a modern transonic fan with compound sweep. ASME J Fluids Eng 134:071101–071107CrossRef
41.
Zurück zum Zitat Gourdain N (2013) Validation of large eddy simulation for the prediction of compressible flow in an axial compressor stage. In: ASME Turbo Expo 2013: turbine technical conference and exposition, volume 6C: turbomachinery, paper GT2013-94550, San Antonio, Texas, USA, 3–7 June Gourdain N (2013) Validation of large eddy simulation for the prediction of compressible flow in an axial compressor stage. In: ASME Turbo Expo 2013: turbine technical conference and exposition, volume 6C: turbomachinery, paper GT2013-94550, San Antonio, Texas, USA, 3–7 June
42.
Zurück zum Zitat Hah C, Hathaway M, Katz J (2014) Investigation of unsteady flow field in a low speed one and a half stage axial compressor: effects of tip gap size on the tip clearance flow structure at near stall operation. In: Proceedings ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2D: turbomachinery, paper GT2014-27094, Düsseldorf, Germany, 16–20 June Hah C, Hathaway M, Katz J (2014) Investigation of unsteady flow field in a low speed one and a half stage axial compressor: effects of tip gap size on the tip clearance flow structure at near stall operation. In: Proceedings ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2D: turbomachinery, paper GT2014-27094, Düsseldorf, Germany, 16–20 June
43.
Zurück zum Zitat Papadogiannis D, Duchane F, Sicot F, Gicquel L, Wang G, Moreau S (2014) Large eddy simulation of high pressure turbine stage: effects of sub-grid scale modeling and mesh resolution. In: Proceedings ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2B: turbomachinery, paper GT2014-25876, Düsseldorf, Germany, 16–20 June Papadogiannis D, Duchane F, Sicot F, Gicquel L, Wang G, Moreau S (2014) Large eddy simulation of high pressure turbine stage: effects of sub-grid scale modeling and mesh resolution. In: Proceedings ASME Turbo Expo 2014: turbine technical conference and exposition, volume 2B: turbomachinery, paper GT2014-25876, Düsseldorf, Germany, 16–20 June
44.
Zurück zum Zitat Hah C (2017) Impact of wake dispersion on axial compressor performance. In: Proceedings ASME Turbo Expo 2017: turbomachinery technical conference and exposition, volume 2A: turbomachinery. Paper GT2017-63020, Charlotte, North Carolina, USA, 26–30 June Hah C (2017) Impact of wake dispersion on axial compressor performance. In: Proceedings ASME Turbo Expo 2017: turbomachinery technical conference and exposition, volume 2A: turbomachinery. Paper GT2017-63020, Charlotte, North Carolina, USA, 26–30 June
45.
Zurück zum Zitat Kemp NH, Sears WR (1955) The unsteady forces due to viscous wakes in turbomachines. J Aeronaut Sci 22:478–483CrossRef Kemp NH, Sears WR (1955) The unsteady forces due to viscous wakes in turbomachines. J Aeronaut Sci 22:478–483CrossRef
46.
Zurück zum Zitat Lowson MV (1968) Reduction of compressor noise radiation. J Acoust Soc Am 43(1):37–50CrossRef Lowson MV (1968) Reduction of compressor noise radiation. J Acoust Soc Am 43(1):37–50CrossRef
47.
Zurück zum Zitat Mailach R, Vogeler K (2002) Experimentelle Untersuchung des instationären Grenzschichtverhaltens auf den Schaufeln eines Niedergeschwindigkeits-Axialverdichters. DGLR Jahrestagung, Paper 2002–071, Deutscher Luft- und Raumfahrtkongress, Stuttgart, Germany, 23–26 September Mailach R, Vogeler K (2002) Experimentelle Untersuchung des instationären Grenzschichtverhaltens auf den Schaufeln eines Niedergeschwindigkeits-Axialverdichters. DGLR Jahrestagung, Paper 2002–071, Deutscher Luft- und Raumfahrtkongress, Stuttgart, Germany, 23–26 September
48.
Zurück zum Zitat Goto S, et al. (2005) Investigation on unsteady loadings due to fan rotor-stator interaction. ISABE symposium on airbreathing engines, paper 2005–1140, Munich, Germany Goto S, et al. (2005) Investigation on unsteady loadings due to fan rotor-stator interaction. ISABE symposium on airbreathing engines, paper 2005–1140, Munich, Germany
Metadaten
Titel
Grundlagen der Aerodynamik
verfasst von
Franz Joos
Copyright-Jahr
2020
DOI
https://doi.org/10.1007/978-3-658-28937-9_2

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