The overall objective of the design effort was to conduct a preliminary vehicle-sizing activity to establish baseline configurations for the STOL tactical aircraft investigation. These preliminary baselines were used for the takeoff and landing studies and as a point of departure for wind tunnel test planning and flight control technology activities. The lift/propulsion concepts studied were: Externally Blown Flap (EBF); Mechanical Flap plus Vectored Thrust (MF/VT); and Internally Blown Flap (IBF). The report summarizes the design activities for the three-month and six-month configuration reviews.
STOL Tactical Aircraft Investigation. Volume I. Configuration Definition
1973
169 pages
Report
Keine Angabe
Englisch
STOL Tactical Aircraft Investigation
SAE Technical Papers | 1973
|Engineering Index Backfile | 1963
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