Aerodynamic test results of controlled pressure ratio engine (cope) dual spool air turbine rotating rig

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Keith, Brian D ^a   Basu, Dipan K ^b   Stevens, Charles ^c  

^a GE AVIATION   (United States)

^b Allison Advanced Development Co   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR ENGINES; AIRCRAFT ACCIDENTS; AIRCRAFT ENGINES; DESIGN; ENGINES; GAS TURBINES; HIGH PRESSURE EFFECTS; MARINE ENGINES; MILITARY AVIATION; NOZZLES; RESEARCH LABORATORIES; SOFTWARE TESTING; TURBINE COMPONENTS; TURBINES; WIND TURBINES;

AERO-DYNAMIC PERFORMANCE; AIR FORCE RESEARCH LABORATORY; COMPONENT EFFICIENCIES; HIGH PRESSURE TURBINE; JOINT STRIKE FIGHTERS; LOW-PRESSURE TURBINES; VARIABLE-CYCLE ENGINES; WRIGHT-PATTERSON AIR FORCE BASE;

AERODYNAMICS;

EID: 84955144925     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0632     Document Type: Conference Paper

References (3)

1. COPE, 1992, "COPE Turbine System Aero Design Validation Program," USAF Contract Number F33615-92-C-2278.
2. CATN, 1992, "CATN Design Program," USAF Contract Number F33615-92-C-2204
3. Doebelin, E.O., 1995, "Engineering Experimentation," McGraw Hill, NY, pp. 64-66.