Veröffentlichungen

1.  Fottner, L.
A Semi-Empirical Approach of the Transonic Flow Past Cascades Including Shock and Viscous Effects
AGARD Conf. Proc. No. 34 (1968)

2.  Fottner, L.
Ein halbempirisches Verfahren zum Bestimmen der reibungsbehafteten transsonischen Schaufelgitterströmung mit Einschluß von Überschallfeldern und Verdichtungsstößen
Dissertation TU München (1970)
Kurzfassung in Forschg. Ing.Wes 36 (1970) Nr.4, S.101-110

3.  Fottner, L.
Ein Verfahren zum Bestimmen der verlustbehafteten transsonischen Schaufelgitterströmung bei vorgegebener Druckverteilung
Forschg.Ing.Wes. 38 (1972) Nr. 3, S. 69 - 81

4.  Fottner, L.
Analytical Approach for the Loss and Deflection Behaviour of Cascades in Transonic Flow Including Axial Mass Flow Variation
AGARDograph No. 164 (1972)

5.  Fottner, L.
Semi-Empirical Methods for Transonic Flow in Turbomachinery
Lecture at VKI short course "Transonic Flow in Turbomachinery"
VKI LS 59 (1973), Brüssel

6.  Volkmann, H., Fottner, L., Scholz, N.
Aerodynamische Entwicklung eines dreistufigen Transonik-Frontgebläses
ZfW 22 (1974), Heft 4, S. 135-144

7.  Fottner, L.
Auslegungsgrundlagen für transsonische Axialverdichter
FVV-Kurzinformation
73/76 (1976)

8.  Fottner, L.
Aerodynamisch hochbelastete Verdichterbeschaufelung mit Grenzschichtbeeinflussung
Forschungsbericht aus der Wehrtechnik BMVg FBWT 77-4 (1977)

9.  Fottner, L.
Theoretical and Experimental Investigations on Aerodynamically Highly-Loaded Compressor Bladings with Boundary-Layer Control
ISABE Orlando, USA (1979)

 10. Fottner, L.
Vorausberechnung des Betriebsverhaltens von transsonischen Axialverdichtern
FVV-Kurzinformation 63/80 (1980)

11. Fottner, L.
Advanced Concepts in Turbomachinery
Lecture Series at the Fluid Dynamic Institute of Dartmouth College, Hanover, N.H. August, 17-21, 1981

12. Fottner, L.
Survey of Models for Shock and Shock/Boundary-Layer Interaction Loss Prediction
AGARD AR 175 (1982)

13. Schäffler, A., Fottner, L.
Survey on the Effects of Blade Surface Roughness on Compressor Performance
AGARD AR 175 (1982)

14. Fottner, L., Lichtfuß, H.-J.
Design of Transonic Compressor Cascades for Minimal Shock Losses and Comparison with Test Results
AGARD Conf. Proc. CP 351 (1983)

15. Fottner, L.
New Design Concepts for Bladings of Axial Turbomachines
15th ICAS Conf. Proc. (1983)

16. Fottner, L.
Überblick über neue Beschaufelungskonzepte
DGLR FA Antriebe (1984)

17. Fottner, L.
Advanced Design Concepts for Axial Compressors and Axial Turbines
Concepts 85. Conf. Proc. (1985)

18. Sturm, W., Fottner, L.
The High-Speed Cascade Wind Tunnel of the German Armed Forces University Munich
8th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Genua, Oct. 1985

19. Neuhoff, F., Shreeve, R.P., Fottner, L.
Evaluation of the Blade-to-Blade Flow from a High-Speed Compressor Rotor
ASME 86-GT-117 (1986)

20. Hoheisel, H., Kiock, R., Lichtfuß, H.J., Fottner, L.
Influence of Free Stream Turbulence and Blade Pressure Gradient on Boundary-Layer and Loss Behaviour of Turbine Cascades
ASME 86-GT-234 (1986)

 21. Genssler,H.P., Meyer,W., Fottner, L.
Development of Intake Swirl Generators for Turbo Jet Engine Testing
AGARD-CP-400 (1986)

22. Römer, N., Ladwig, M., Fottner, L.
Measuring Techniques at the High-Speed Cascade Windtunnel of the University of the Federal Armed Forces Munich
9th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Oxford, March 1988

23. Fottner, L. (Edt.)
Blading Design for Axial Turbomachines
AGARD-LS-167 (1989)

24. Fottner, L.
Review of Turbomachinery Blading Design Problems
AGARD-LS-167 (1989)

25. Fottner, L.
Overview on Test Cases for Computation of Internal Flows in Turbomachines
ASME 89-GT-46 (1989)

26. Fottner, L. (Edt.)
Test Cases for Computation of Internal Flows in Aero Engine Components
AGARD-AR-275 (1990)

27. Pazur, W., Fottner, L.
The Influence of Inlet Swirl Distortions on the Performance of a Jet Propulsion Two-Stage Axial Compressor
ASME 90-GT-147 (1990)

28. Wilfert, G., Ladwig, M., Fottner, L.
PANDA - A new Data Acquisition System for Wake and Profile Pressure Distribution Measurements at the High-Speed Cascade Wind Tunnel
10th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Brussel, Sep-tember 1990

29. Watzlawick, R., Fottner, L.
Bestimmung der wesentlichen Einflußgrößen in der Korrelation der Sekundärströmungsverluste bei Veränderung des Schaufelseitenverhältnisses
FVV Heft R 482 (1991)

30. Sturm, W., Scheugenpflug, H., Fottner, L.
Performance Improvements of Compressor Cascades by Controlling the Profile and Sidewall Boundary-Layers
ASME 91-GT-260 (1991)

31. Berns, W., Fottner, L.
Experimental Analysis of the Dynamic Performance of Turbojet Engines
ISABE Nottingham (1991)

32. Meyer, W., Pazur, W., Fottner, L.
The Influence of Intake Swirl Distortion on the Steady-State Performance of a Low Bypass, Twin-Spool Engine
AGARD CP-498 (1991)

33. Watzlawick, R., Fottner, L.
Bestimmung der wesentlichen Einflußgrößen in der Korrelation der Sekundärströmungsverluste bei Veränderung des Schaufelseitenverhältnisses
MTZ 53, Heft 6 (1992)

34. Fottner, L. (Edt.)
Steady and Transient Perfomarmance Prediction of Gas Turbine Engines
AGARD LS 183 (1992)

35. Wunderwald, D., Wilfert, G., Fottner, L.
The Experimental Set-Up of a Triple-Sensor Anemometry and its Controlling System at the High-Speed Cascade Wind Tunnel
11th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Neubiberg, September 1992

36. Beeck, A., Fottner, L., Benz, E., Wittig, S.
The Aerodynamic Effect of Coolant Ejection in the Leading Edge Region of a Film Cooled Turbine Blade
AGARD CP 527 (1992)

37. Fottner, L. (Edt.)
Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines
Conference Proceedings, Neubiberg, 1993

38. Weiß, A.P., Fottner, L.
Die Auswirkungen unterschiedlicher Belastungsverteilungen von Turbinengittern auf die Energiedissipation und auf die Verteilung der Verluste und des Abströmwinkels über der Schaufelhöhe
DGLR-Fachausschuß-Sitzung Uni Stuttgart, 1993

39. Benz, E., Wittig, S., Beeck, A., Fottner, L.
Analysis of Cooling Jets near the Leading Edge of Turbine Blades
AGARD CP 534 (1993)

40. Weiß, A.P., Fottner, L.
The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades
ASME 93-GT-86 (1993)
Journ. of Turbomachinery Vol. 117 No. 1 (1995) pp 133-141

41. Sachmann, J., Fottner, L.
Highly Loaded Tandem Compressor Cascade with Variable Camber and Stagger
ASME 93-GT-235 (1993)

42. Ladwig, M., Fottner, L.
Experimental Investigations of the Influence of Incoming Wakes on the Losses of a Linear Turbine Cascade
ASME 93-GT-394 (1993)

43. Herpel, Th., Fottner, L.
A System for Monitoring, Measurement and Analysis of Transient Performance and Stall Phenomena of Gas Turbine Engines
Conf.Proc. Instrumentation in Aerospace Facilities, Saint-Louis (1993)

44. Bernhard, D., Fottner, L.
Einfluß kombinierter Drall- und Totaldruck-Eintrittsstörungen auf das Stabilitätsverhalten von Turbostrahltriebwerken
DGLR Jahrestagung Göttingen DGLR-JT93-047 (1993)

45. Hildebrandt, Th., Fottner, L.
Durham Low Speed Turbine Cascade - 3D-Navier-Stokes Calculation
ERCOFTAC Workshop 10-13 January 1994, Val d'Isere (1994)

46. Wilfert, G., Fottner, L.
The Aerodynamic Mixing Effect of Discrete Cooling Jets with Mainstream Flow on a Highly Loaded Turbine Blade
ASME 94-GT-235 (1994)
Journ. of Turbomachinery Vol. 118 No. 3 (1996) pp 468-478
 

47. König, W.M., Hennecke, D.K., Fottner, L.
Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings
Part I: A Model for Subsonic Flow
ASME 94-GT-335 (1994)

48. König, W.M., Hennecke, D.K., Fottner, L.
Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings
Part II: A Model for Supersonic Flow
ASME 94-GT-336 (1994)

49. Acton, P., Fottner, L.
The Generation of Isotropic Turbulence in the High Speed Cascade Wind Tunnel
12th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Prague, September 1994

50. Bell, R.M., Fottner, L.
Schlieren Method with Quantitative Evaluation by Digital Image Processing
12th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Prague, September 1994

51. Engber, M., Fottner, L.
The Effect of Incoming Wakes on Boundary Layer Transition of a Highly Loaded Turbine Cascade
AGARD CP 571 (1995)
 

52. Bell, R.M., Fottner, L.
Investigations of Shock/Boundary-Layer Interaction in a Highly Loaded Compressor Cascade
ASME 95-GT-84 (1995)

53. Wunderwald, D., Fottner, L.
Experimental Investigation of Boundary Layer Transition and Turbulence Structures on a Highly Loaded Compressor Cascade
ASME 95-GT-129 (1995)

54. Hu, J., Fottner, L.
Calculations of Effects of Rotating Inlet Distortion on Flow Instabilities in Compression Systems
ASME 95-GT-196 (1995)

55. Wilfert, G., Fottner, L.
Mischungsvorgänge zwischen Kühlfilmen und Gitterströmung an einem hochbelasteten Turbinengitter
DGLR FA TU Berlin (1995)

56. Ardey, S., Fottner, L.
Strömungssichtbarmachung und Untersuchungen zum Verlustverhalten an einem Turbinenschaufelgitter mit Vorderkanten-Fimkühlung
DGLR FA TU Berlin (1995)

57. Vogel, D.T., Wilfert, G., Fottner, L.
Numerical and Experimental Investigations of Film Cooling from a Row of Holes at the Suction Side of a Highly Loaded Turbine Blade
ISABE Melbourne (1995)

58. Herpel, Th., Fottner, L.
Transient Performance of Turbofan Engines with Respect to Unsteady Compressor Flow near the Stability Limit
ISABE Melbourne (1995)

59. Müller, J.E., Fottner, L.
Numerische und experimentelle Untersuchung des Strömungsfeldes im Einlaufkanal eines Hyperschall-Kombinationstriebwerks
DGLR Jahrestagung Bonn DGLR-JT95-072 (1995)

60. Müller, J.E., Fottner, L.
Numerical and Experimental Investigations of the Flow Field Inside the Intake Duct of a Combined Cycle Engine for Hypersonic Flight
Proc. of ASME Conf. on "Computational Fluid Dynamics in Aeropropulsion", San Francisco (1995)

61. Hildebrandt, Th., Fottner, L.
Durham Low Speed Turbine Cascade - Test Case 3
ERCOFTAC Workshop 08-11 January 1996, Courchevel (1996)

62. Wunderwald, D., Fottner, L.
Experimental Investigation of Turbulence Structures in the Boundary Layer of a Highly Loaded Turbine Cascade
ASME 96-GT-249 (1996)

 63. Hübner, J., Fottner, L.
Influence of Tip Clearance, Aspect Ratio, Blade Loading and Inlet Boundary Layer on Secondary Losses in Compressor Cascades
ASME 96-GT-505 (1996)

64. Acton, P., Fottner, L.
The Generation of Instationary Flow Conditions in the High Speed Cascade Wind Tunnel
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, Sep-tember 1996

65. Ganzert, W., Fottner, L.
WINPANDA - An Enhanced PC-Based Data Acquisition System for Wake and Profile Pressure Distribution Measurements at the High Speed Cascade Wind Tunnel
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, September 1996

66. Jahnen, W., Fottner, L.
A New Multi-Stage Compressor Test Facility for Inlet Distortion Investigations
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, September 1996

67. Hildebrandt, Th., Fottner, L.
Numerische Untersuchung der Strömung in einem hochbelasteten Axialverdichter mit unterschiedlichen 3D Navier-Stokes Verfahren
DGLR Jahrestagung Dresden (1996)

68. Ardey, S., Fottner, L.
Messungen an einer filmgekühlten Turbinenschaufelvorderkante
5. Statusseminar AG TURBO DLR Köln (1996)

69. Duden, A., Fottner, L., Braig, W., H.-F. Vogt, Raab, I.,
Sauer, H.
Messungen an einer filmgekühlten Turbinenschaufelvorderkante
5. Statusseminar AG TURBO DLR Köln (1996)

70. Hu, J., Fottner, L.
Numerical Simulation of Active Suppression of Rotating Stall in Axial Compression Systems
Journ. of Thermal Science Vol. 5, No. 4, pp 231-242 (1996)

71. Duden, A., Fottner, L.
Influence of Taper, Reynolds Number and Mach Number on the Secondary Flow of a Highly Loaded Turbine Cascade
Conf. Proc. of 2nd European Conference on Turbomachinery,
5-7 March, Antwerpen (1997)

72. Fottner, L. (Edt.)
Design of Aero Engines for Safety, Reliability, Maintainability and Cost
Conference Proceedings of the 1997 European Propulsion Conference, Berlin, (1997)
73. Ardey, S., Fottner, L.
Flow Field Measurements on a Large Scale Turbine Cascade with Leading Edge Film Cooling by Two Rows of Holes
ASME 97-GT-524 (1997)

74. Bohn, D., Becker, V., Kusterer, K., Ardey, S. Fottner, L.
The Influence of Slot Ejection and Showerhead Ejection on the 3D Flowfield of a Film-Cooled Turbine Blade under Consideration of Side Wall Effects
ISABE Chattanooga, USA (1997)

75. Schnaus, J., Fottner, L.
Experimental and Numerical Investigations of the Influence of Endwall-Inclination and Contouring on the Flow Field in a Highly Loaded Turbine Cascade
ISABE Chattanooga, USA (1997)

76. Acton, P., Fottner, L.
Investigation of the Boundary Layer Development on a Highly Loaded Low Pressure Turbine Cascade under the Influence of Unsteady Flow Conditions
8th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm, Sweden (1997)

77. Jahnen, W., Peters, Th., Fottner, L.
An Experimental Flow Investigation of an HP Five-Stage Compressor Exhibiting Rotating Stall due to Distorted Inlet Flow Conditions
8th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm, Sweden (1997)

78. Ganzert, W., Fottner, L.
Set-Up of a Heat Transfer Coefficient Measurement System at the High Speed Cascade Wind Tunnel
Eurotherm Seminar No. 55 on "Heat Transfer in Single Phase Flows", Santorin, Greece (1997)

79. Höss, B., Fottner, L.
Experimental Set-Up, Measurement and Analysis of the Onset of Compressor Flow Instabilities in an Aero Engine
17th Int. Congr. on Instrumentation in Aerospace Simulation Facilities, Monterey, USA (1997)

80. Leinhos, D., Höss, B., Fottner, L.
Rotating Stall Inception with Inlet Distortion in the Low Pressure Compressor of a Turbofan Engine
19th Int. Symp. Aircraft Integrated Monitoring Systems, May 1998 Garmisch-Partenkirchen (1998)

81. Ardey, S., Fottner, L.
A Systematic Experimental Study on the Aerodynamics of Leading Edge Film Cooling on a Large Scale High Pressure Turbine Cascade
ASME 98-GT-434 (1998)

82. Dohring, Cl., Fottner, L., Platzer, M.F.
Experimental and Numerical Investigations of Flapping Wing Propulsion and its Application for Boundary-Layer Control
ASME 98-GT-046 (1998)

83. Duden, A., Raab, I., Fottner, L.
Controlling the Secondary Flow in a Turbine Cascade by 3D Airfoil Design and Endwall Contouring
ASME 98-GT-072 (1998)

84. Hildebrandt, Th., Fottner, L.
A Numerical Study of the Influence of Grid Refinement and Turbulence Modelling on the Flow Field inside a Highly Loaded Turbine Cascade
ASME 98-GT-240 (1998)

85. Höss, B., Leinhos, D., Fottner, L.
Stall Inception in the Compressor System of a Turbofan Engine
ASME 98-GT-475 (1998)

86. Brunner, S., Teusch, R., Stadtmüller, P., Fottner, L.
The Use of Simultaneous Surface Hot Film Anemometry to Investigate Unsteady Wake Induced Transition in Turbine and Compressor Cascades
14th Symposium on Measuring Techniques for Transonic and Su-personic Flow in Cascades and Turbomachines, Limerick, September 1998

87. Leipold, R., Fottner, L.
A Measurement Technique to Investigate the Influence of Surface Roughness on the Flow around a Highly Loaded Compressor Cascade
14th Symposium on Measuring Techniques for Transonic and Su-personic Flow in Cascades and Turbomachines, Limerick, September 1998

88. Schmid, N., Hildebrandt, Th., Fottner, L.
Numerical Investigations of the Flow Field Inside the Intake Diffuser of a Combined Cycle Engine for Hypersonic Flight
4th ECCOMAS Computational Fluid Dynamics Conference, Athens, September 1998

89. Ganzert, W., Fottner, L.
Untersuchungen des Wärmeübergangs an einem filmgekühlten Turbinengitter im Hochgeschwindigkeits-Gitterwindkanal
DGLR Jahrestagung 1998, Bremen

90. Swoboda, M., Teusch, R., Fottner, L., Gümmer, V., Wenger, U.
Experimentelle Untersuchung zum Transitionsverhalten in Verdichtergittern mit periodisch veränderlicher Zuströmung
STAB Fachsymposium Berlin, 1998

91. Brunner, S., Fottner, L., Schulte, V., Kappler, G.
Investigation of Wake-Induced Transition on a Highly Loaded Low Pressure Turbine Cascade
Conf. Proc. of 3nd European Conference on Turbomachinery, 2-5 March 1999 C557/068/99, London, UK (1999)

92. Brunner, S., Teusch, R., Fottner, L., Schiffer, H.-P., Swoboda, M.
Optimierung hochbelasteter Turbinen- und Verdichterbeschaufelungen mit Berücksichtigung instationärer Zuströmung
6. Statusseminar AG TURBO DLR Köln (1998)

93. Wolff, St., Ardey, S., Fottner, L.
Proposal for a New ERCOFTAC Test Case: Leading Edge Film Cooling on a Large High Pressure Turbine Cascade
ERCOFTAC Workshop 04-07 January 1999, Aussois (1999)

94. Schwarz, C., Schmid, N. Fottner, L.
Model Wind-Tunnel Tests for the Optimisation of the Flow Field inside the Subsonic Diffuser of an Intake for a Combined Cycle Engine for Hypersonic Flight
Conference Proceedings of the 1999 European Propulsion Forum, Pau, France, (1999)

95. Leipold, R., Boese, M., N. Fottner, L.
The Influence of Technical Surface Roughness on the Flow around a Highly Loaded Compressor Cascade
ASME 99-GT-366 (1999)
Journal of Turbomachinery Vol. 122 No. 3 416-425

96. Jahnen, W., Peters, T., Fottner, L.
Stall Inception in a 5 stage HP Compressor with Increased Load Due to Inlet Distortion
ASME 99-GT-440 (1999)

97. Ganzert, W., Fottner, L.
Film Cooling Over a Concave Surface Through a Row of Expanded Holes
ASME 99-GT-039 (1999)

98. Duden, A., Fottner, L.
The Secondary Flow Field of a Turbine Cascade with 3D Airfoil Design and Endwall Contouring at Off-Design Incidence
ASME 99-GT-211 (1999)

99. Teusch, R., Fottner, L., Swoboda, M.
Experimental Investigation of Wake-Induced Transition in a Linear Compressor Cascade with Controlled Diffusion Blading
ISABE Paper IS-7057, Florenz, Italy (1999)

100. Leipold, R., Boese, M., Fottner, L.
The Influence of Technical Surface Roughness of Modern Blade Manufacturing Methods on the Flow Around a Compressor Cascade
ISABE Paper IS-7019, Florenz, Italy (1999)

101. Schmid, N.R., Leinhos, D.C., Fottner, L.
Performance of a Turbofan Engine with Inlet Distortions from the Intake Diffuser of a Combined Cycle Engine for Hypersonic Flight
ISABE Paper IS-7076, Florenz, Italy (1999)

102. Brunner, S., Fottner, L.
Untersuchungen zum Einfluß der Rotor/Stator-Interaktion auf die saugseitige Transition eines hochbelasteten ungekühlten Niederdruck-Turbinengitters
DGLR Jahrestagung 1999, Berlin

103. Hu, J., Peters, Th., Fottner, L.
Numerical Simulation of Flow Instabilities in High Speed Multistage Compressors
Journ. of Thermal Science Vol. 8, No. 1, pp 23-31 (1999)

104. Brunner, S. Müller, P., Fottner, L.
Turbomachichery Research at the Jet Propulsion Institute of the University of the Federal Armed Forces Munich
ERCOFTAC Bulletin No. 42,(1999), pp 19-30

105. Leinhos, D., Peters, Th., Fottner, L.
Verfahren zur Früherkennung von Verdichterinstabilitäten am Beispiel des ND-Verdichters eines Turbofan-Triebwerks
DGLR-Fachausschuß-Sitzung RWTH Aachen, 2000

106. Brandt, H., Fottner, L.
Investigations of the Aerodynamics and the Heat Transfer on the Suction Side of the Film Cooled Turbine Cascade T106-300
ERCOFTAC Workshop 19-23 March 2000, la Clusaz (2000)

107. Kampitsch, M., Stadtmüller, P., Fottner, L.
Investigations of Wake-Induced Transition on the LPT Cascades T106A-EIZ and T106D-EIZ
ERCOFTAC Workshop 19-23 March 2000, La Clusaz (2000)

108. Leinhos, D.C., Schmid, N.R., Fottner, L.
The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine
ASME 2000-GT-0505 (2000)

109. Wolff, St., Brunner, St., Fottner, L.
The Use of Hot-Wire Anemometry to Investigate Unsteady Wake-Induced Boundary-Layer Development on a High Lift LP Turbine Cascade
ASME 2000-GT-0049 (2000)

110. Teusch, R. Brunner, St., Fottner, L. ,Swoboda, M.
The Influence of Multimode Transition Initiated by Periodic Wakes on the Profile Loss of a Linear Compressor Cascade
ASME 2000-GT-0271 (2000)

111. Ardey, S., Wolff, St., Fottner, L.
Turbulence Structures of Leading Edge Film Cooling Jets
ASME 2000-GT-0255 (2000)

112.Ganzert, W., Fottner, L., Hildebrandt, Th.
Systematic Experimental an Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape - Part I: Experimental Approach
ASME 2000-GT-0295 (2000)

113. Ganzert, W., Fottner, L., Hildebrandt, Th.
Systematic Experimental an Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape - Part II: Numerical Approach
ASME 2000-GT-0298 (2000)

114. Schmid, N.R., Leinhos, D.C., Fottner, L.
Steady Performance Measurements of a Turbofan Engine with Inlet Distortions Containing Co- and Counter-Rotating Swirl from an Intake Diffuser for Hypersonic Flight
ASME 2000-GT-0011 (2000)

115. Stadtmüller, P., Fottner, L., Fiala, A.
Experimental and Numerical Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine Cascade at Low Reynolds Numbers
ASME 2000-GT-0269 (2000)

116. Brandt, H., Ganzert, W., Fottner, L.
A Presentation of Detailed Experimental Data of a Suction Siede Film Cooled Turbine Cascade
ASME 2000-GT-0296 (2000)

117. Teusch, R., Kampitsch, M., Th., Fottner, L.
Experimental and Numerical Investigations of the Flow Behaviour in Compressor Cascades under the Influence of Wakes
9th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Lyon, France (2000)

118. Boese, M., Fottner, L.
Einfluss widerstandsreduzierender Oberflächenstrukturen auf das Verlustverhalten eines aerodynamisch hochbelasteten Verdichtergitters
DGLR Jahrestagung 2000, Leipzig

119. Hildebrandt, Th., Ganzert, W., Fottner, L.
Numerische Simulation eines filmgekühlten Turbinengitters mit einer Variation der Ausblasebohrungen
DGLR Jahrestagung 2000, Leipzig

120. Stadtmüller, P., Fottner, L.
Fast Response Pressure Transducers for the Inverstigation of Wake-Induced Transition on a Highly Loaded LP Turbine
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, Sep-tember 2000

121. Peters. Th., Fottner, L.
A Coupled Steady-Unsteady-State Data Acquisition System for the Investigation of Rotating Inlet Distortions at a Mult-Stage Compressor Test Facility
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, Sep-tember 2000

122. Wolff, St., Fottner, L.
Glue-On Hot Film Sensors to Investigate Heat Transfer on a Highly Loaded LP Film-Cooled Turbine Blade
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, Sep-tember 2000

123. Gier, J., Braig, W.,Niehuis, R.,Schodl, R., Fottner, L.
Seitenwandkonturierung in Turbinengittern
7. Statusseminar AG TURBO DLR Köln (2000)

124. Schiffer, H.P., Haselbach, F.,Fottner, L.
Hochbelastete ungekühlte Turbinenbeschaufelung
7. Statusseminar AG TURBO DLR Köln (2000)

125. Wolff, S., Fottner, L.
Vorderkantenausblasung bei periodisch instationärer Zuströmung
7. Statusseminar AG TURBO DLR Köln (2000)

126. Peters, Th., Bürgener, Th., Fottner, L
Stall Inception in a 5-Stage HP-Compressor under the Influence of Rotating Inlet Distortion
Conf. Proc. of 4th European Conference on Turbomachinery, 20-23 March 2001, Florence, Italy (2001)

127. Wolff, St., Homeier, L., Fottner, L.
Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded Turbine Cascade
Conf. Proc. of RTO/AVT Symposium 7-11 May 2001 Loen, Norway

128. Peters, T., Fottner, L.
Effects of Rotating Inlet Distortion on a 5-stage HP Compressor
ASME 2001-GT-0300 (2001)

129. Stadtmüller, P., Fottner, L.
A Test Case for the numerical Investigation of Wake-Passing Effects on a Highly Loaded LP Turbine Cascade
ASME 2001-GT-0311 (2001)

130. Leinhos, D.C., Scheidler, St., Fottner, L.
Active Stabilization of a Low Pressure Compressor in a Turbofan Engine with Constant Air Injection
AIAA 2001-3312 (2001)

131. Nagel, M.G., Fottner, L., Baier, R.D.
Optimization of Three-Dimensionally Designed Turbine Blades and Side Walls
ISABE IS-2001-1058 (2001)

132. Kampitsch, M., Fottner, L.
Vergleich unterschiedlicher Mehtoden zur Berechnung der Nachlauf/Grenzschicht-Interaktion in einem hoch belasteten Turbinenschaufelgitter
DGLR JT 2001 Hamburg(2001)

133. Scheidler, St., Fottner, L.
Das dynamische Betriebsverhalten eines Turbostrahltriebwerks bei Einlaufstörungen und reduziertem Pumpgrenzabstand
DGLR-Jahrestagung 2001-205 (2001)

134. Boese, M., Fottner, L.
Einfluß von Ribletstrukturen auf das Verlustverhalten eines aerodynamisch hochbelasteten Verdichtergitters
TU Dresden Conf. Proc. (2001)

135. Boese M., Fottner L.,: Untersuchungen an widerstandsreduzierenden Oberflächenstrukturen für Verdichterbeschaufelungen
Vortrag im Seminar Flugantriebe und Gasturbine, TU Mün-chen, Garching, 31. Januar 2002, bei Rolly Royce Deutschland am 02.10.02

136. Boese M., Fottner L.
Effects of Riblets on the Loss Behavior of a Highly Loaded Compressor Cascade
ASME TURBO EXPO 2002, 03. - 06.06.2002

137. Brandt, H., Fottner, L., Saathoff H., Stark U.: Effects of the Inlet Flow Conditions on the Tip Clearance Flow of an Isolated Rotor
ASME TURBO EXPO 2002, 03. - 06.06.2002

138. Cardamone P., P. Stadtmüller, Fottner L.
Numerical Investigation Of The Wake-Boundary Layer Interaction On A Higly Loades LP Turbine Cascade Blade
ASME TURBO EXPO 2002, 03. - 06.06.2002

139. Hoeger M., Cardamone P., Fottner L.
 Influence Of Endwall Contouring On The Transonic Flow In A Compressor Blade
ASME TURBO EXPO 2002, 03. - 06.06.2002

140. Leinhos D., Scheidler St., Fottner L.: Experiments In Active Stall Control Of A Twin-Spool Turbofan Engine
GT-2002-30002, ASME TURBO EXPO 2002, 03. - 06.06.2002

141. Wolff St., Ardey S. Fottner L.
An Experimental Investigation On The Influence Of Periodic Unsteady Inflow Conditions On Leading Edge Film Cooling
ASME TURBO EXPO 2002, 03. - 06.06.2002

142. Hilgenfeld, L., Fottner L.
Experimental investigation of turbulence structures in a highly loaded transonic compressor cascade with schock / laminar boundary layer interactions
5th Symp. on Engineering Turbulence Modelling and Measurements, Mallorca, Spain, 16-18 September 2002

143. Schwarz, C.: Aerodynamische Untersuchung eines typischen Abblase-Luftsystems in einem mehrstufigen_Axialverdichters.
DGLR - Jahresband, Teil II, 2002

144. Hilgenfeld, L.; Stadtmüller, P.; Fottner, L.
Experimental Investigation of turbulence influence of wake passing on the boundary layer developement of highly loaded turbine cascade blades.
Journal of Flow, Turbulence and Combustion, Vol. 69 (3-4), Seiten 229-247, 2002

145. Wolff St., Fottner L.
Experimentelle Untersuchung zum Einfluß von periodisch instationärer Zuströmung auf das 3D Strömungsfeld einer Film-gekühlten Hochdruckturbinenschaufel
DGLR Paper DGLR-2002-072 , Stuttgart/Deutschland, 2002

146. Wolff St., Fottner L.
Vorderkantenausblasung bei periodisch instationärer Zuströmung
8. Stausseminar der AG TURBO Köln/Deutschland, 2002

147. Hilgenfeld, L., Cardamone, P., Fottner, L.
Boundary Layer Investigations in a Highly Loaded Transonic Compressor Cascade with Shock/ Laminar Boundary Layer Interactions
5th European Conference on Turbomachinery, Prag, 2003

148. Schwarz, C., Brandt, H., Fottner, L.
Doppler Global Velocimetry Messungen in einem Verteilerkanal eines typischen Abblase-Luftsystems in einem mehrstufigen Axialverdichter
GALA Tagung "Lasermethoden in der Strömungsmesstechnik", Braunschweig, 2003

149. Schwarz, C., Brandt, H., Fottner, L.
Optimale Abblasekonfigurationen in mehrstufigen Axialverdichter
Abschlussbericht, FVV-Informationtagung Turbinen, Magdeburg, 2003

150. Brandt H., Schwarz C., Fottner L.
Verschiedene Ansätze zur Untersuchung einer typischen Verdichter-Luftabblasung --Nachrechnung experimenteller Ergebnisse
DGLR-Workshop "Luftsysteme in Flugzeugen und Triebwerken", DGLR-Bericht 2003-03, Ottobrunn, 2003

151. Brandt H., Schwarz C., Fottner L.
Numerische Untersuchung des dreidimensionalen Strömungsfeldes eines typischen Abblase-Luftsystems mehrstufiger Axialverdichter
XXXV. Kraftwerktechnisches Kolloquium, Dresden, 2003

152. Scheidler, S., Fottner, L.:
Active Stabilization of the Compression System in a Twin-spool Turbofan Engine at Inlet Distortions
ISABE-2003-1083, XVI. ISABE, Cleveland, Ohio, USA, 2003

153. Scheidler, S., Fottner, L.:
Operational Characteristics of a Twin-spool Turbofan Engine at Inlet Distortions with Reduced Surge Margin
RTO-AVT-2003-029, RTO-AVT-100 Symposium, Warschau, Polen, 2003.

154. Hilgenfeld, L., Pfitzner, M.:
Experimental Investigation of Wake-Induced Transition in a Highly Loaded Linear Compressor Cascade
10. ISUAAAT, Durham, NC, USA, 2003

155. Hilgenfeld, L., Brandt, H., Pfitzner, M.:
Untersuchung des Grenzschicht- und Turbulenzverhaltens eines hochbelasteten Transsonik-Verdichtergitters mit Verdichtungsstoß-Grenzschicht-Interaktion.
Deutsche Luft- und Raumfahrtkongress, München, 17.-20. November 2003

156. Homeier, L., Pfitzner, M., Haselbach, F., Schiffer, H. P. :
"Experimentelle Untersuchungen an einem
hochbelasteten Hochdruckturbinengitter ohne
und mit saugseitiger Filmkühlung"
DGLR-2003-201, Jahrbuch 2003, Band III
DGLR Jahrestagung 2003, 17./20. November 2003, München

157. Scheidler S.G., Mundt, C.:
"Active Stability Control Of The Compression System In A Twin-Spool Turbofan Engine By Air Injection"
ISROMAC 10-2004-073, The 10th of International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, USA, March 07-11, 2004.

158. Hummel, F., Lötzerich, M., Cardamone, P., Fottner, L. :
"Surface Roughness Effects on Turbine Blade Aerodynamics",
GT-2004-53314, ASME Turbo Expo 2004, June 14-17 2004 Vienna
(published in the "Journal of Turbomachinery", Vol. 127, Juli 2005)

159. Scheidler, S.G.; Fottner, L.:
"Experimental Operating Range Extension Of A Twin-Spool Turbofan Engine By Active Stability Control Measures"
GT-2004-53077, ASME Turbo Expo 2004, June 14-17, 2004 Vienna
(published as GTP-04-1043 in the "Journal of Engineering for Gas Turbines and Power", Vol. 127, October 2005)

160. Hilgenfeld, L.; Pfitzner, M.:
Unsteady boundary layer developement due to wake passing effects on a highly loaded linear compressor cascade.
ASME Turbo-Expo Wien, 14.-17. Juni 2004
(published in the "Journal of Turbomachinery", Vol. 126, pp. 493-500, 2004)

161. Cardamone, P.; Pfitzner, M.; Lötzerich, M.:
"Aerodynamische Optimierung hochbelasteter Hochdruckturbinengitter"
DGLR-2004-225, Jahrbuch 2004, Band I, II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden

162. Hilgenfeld, L.; Iseler, J.; Pfitzner, M.:
"Einfluss von periodisch instationären Zuströmbedingungen auf das instationäre Grenzschichtverhalten eines hoch belasteten Verdichtergitters."
DGLR-2004-227, Jahrbuch 2004, Band I,II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden

163. Reuss, N.; Mundt, C.:
"Experimentelle Untersuchungen zum Einfluß kombinierter Eintrittstotaldruckstörungen auf das Betriebsverhalten des fünfstufigen Hochdruckverdichters Rig212"
DGLR-2004-122, Jahrbuch 2004, Band I,II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden

164. Homeier, L., Lutum, E., Janke, E., Haselbach, F. :
"Aero-Thermodynamic Aspects of Film Cooling in Regions of
Separated Flow on the Pressure Side of a High-Lift HPT Blade"
GT-2004-54067, ASME Turbo Expo 2004, June 14-17 2004 Vienna

165. Cardamone, P., Pfitzner, M., Lötzerich, M. :
"Aerodynamic optimisation of a HP turbine cascade blade for heavy-duty gas turbine applications"
6th European Conference on Turbomachinery (ETC 6), 7-11 March 2005, Lille, France

166. Homeier, L., Haselbach, F. :
"Impact of suction side cooling on the losses of a highly loaded high pressure turbine blade"
6th European Conference on Turbomachinery (ETC 6), 7-11 March 2005, Lille, France

167. Homeier, L.; Haselbach, F.:
"Film Cooling of Highly Loaded Blades"
AIAA-2005-1114, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich

168. Gomes, R.A.; Schwarz, C.; Pfitzner, M.:
"Aerodynamic Investigations of a Typical Configuration for Bleed Flow in Aeroengines"
AIAA-2005-1264, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich

169. Cardamone, P.; Martinstetter, M.; Pfitzner, M.; Lötzerich, M.:
"Aerodynamic Optimisation of Highly-Loaded HP Turbine Blades for Heavy Duty Gas Turbines"
AIAA-2005-1257, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich

170. Scheidler, S.; Mundt, C.:
"Fatal Damage of a Twin-Spool Turbofan Engine due to Fan Blade Off"
AIAA-2005-1206, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich

171. Iseler, J.; Hilgenfeld, L.; Pfitzner, M.:
"Unsteady Boundary Layer Development due to Wake Passing Effects on a Highly Loaded Linear Compressor Cascade"
AIAA-2005-1054, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich

172. Pfitzner, M.; Gomes, R.; Schwarz, C.:
"Optimale Auslegung von Luftsystemen am Beispiel der Abblase-Konfiguration mehrstufiger Axialverdichter II"
FVV-Informationstagung Turbinen, 28. Sept. 2005, Köln, Heft R532 (2005)

173. Gomes, R.; Schwarz, C.; Pfitzner, M.:
"Experimental Investigation of a Generic Compressor Bleed System"
GT2006-90458, ASME TurboExpo, Barcelona, 2006

174. Iseler, J.; Hilgenfeld, L.; Pfitzner, M.:
"Investigations of the Boundary Layer on a highly loaded Compressor Cascade with wake-induced Trasition"
GT2006-90665, ASME TurboExpo, Barcelona, 2006

175. Scheidler, S. G.; Bindl, S.; Mundt, C.:
"Mapping the Control Parameters of an analog Fuel Control to prepare for the retrofit of a Digital Control Unit"
GT2006-90126, ASME TurboExpo, Barcelona, 2006