Preparatory to developing mission profiles for future attack, crane, observation, assault, transport, and utility helicopters, the flight condition recognition (FCR) technique was applied to some 10-hour data samples for each of the following class-model helicopters which had acquired 200 or more hours of multichannel oscillograph data during operational usage surveys while the helicopters operated under combat conditions in Southeast Asia (SEA): attack - AH-1G, crane - CH-54A, observation - OH-6A, assault - UH-1H, transport - CH-47A, and utility - UH-1H.
Dynamic Loads and Structural Criteria
1975
200 pages
Report
No indication
English
Aircraft , Aeronautics , Helicopters , Mission profiles , Flight envelope , Flight maneuvers , Combat surveillance , Aircraft landings , Takeoff , Level flight , H-1 aircraft , AH-1G aircraft , Huey Cobra , H-47 aircraft , CH-47A aircraft , H-54 aircraft , CH-54A aircraft , H-6 aircraft , OH-6A aircraft , UH-1H aircraft
Dynamic Loads and Structural Criteria Study
NTIS | 1974
|Thermal-Structural Combined Loads Design Criteria Study
NTIS | 1972
|Thermal-structural combined loads design criteria study
TIBKAT | 1972
|Thermal-structural combined loads design criteria study
NTRS | 1972
|