[ASME ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition - Houston, Texas, USA (Monday 5 June 1995)] Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration - Adiabatic Effectiveness, Thermal Fields, and Velocity Fields for Film Cooling With Large Angle Injection
- 作者Kohli, Atul; Bogard, David G.
- 文件大小753.24KB
- 发表时间1995
- DOI10.1115/95-gt-219
[ASME ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition - Cincinnati, Ohio, USA (Monday 24 May 1993)] Volume 3C: General - GETRAN: A Generic, Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero- and Power Generation Gas Turbine EnginesSchobeiri, T.; Abouelkheir, M.; Lippke, C. · 1993
[ASME ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition - Cincinnati, Ohio, USA (Monday 24 May 1993)] Volume 3A: General - The Effects of Scale Factor on the Aero-Thermodynamic and Infrared Radiation Performance of Naval Gas Turbine Exhaust System With Infrared Signature Suppression DeviceZhong, Fangyuan; Dai, Yu · 1993
[ASME ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition - Cincinnati, Ohio, USA (Monday 24 May 1993)] Volume 3A: General - Influence of High Rotational Speeds on Heat Transfer and Oil Film Thickness in Aero Engine Bearing ChambersWittig, S.; Glahn, A.; Himmelsbach, J. · 1993