Preliminary designs are developed for five V/STOL 10-ton cargo transports capable of 1800 nautical mi range; peak loads and stresses are calculated from structural dynamic response to ground handling, flight maneuver, gust penetration, and landing; loads and stresses are compared to those used to originally design aircraft; results are tabulated in matrix showing degree of relative criticalness for conditions investigated for each V/STOL configuration.
Structural dynamic response of large logistic V/STOL aircraft
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 12 , n 4 ; p 22-37
1967
16 pages
Article (Journal)
English
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V/STOL aircraft structural considerations
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