Takeoff and landing performance characteristics and field length requirements were determined analytically for a jet STOL transport configuration with full-span, externally blown, tripleslotted flaps. The configuration had a high wing, high T-tail, and four pod-mounted high-bypass-ratio turbofan engines located under and forward of the wing. One takeoff and three approach and landing flap settings were evaluated. The effects of wing loading, thrust-to-weight ratio, weight, ambient temperature, altitude on takeoff and landing field length requirements are discussed.
Analytical study of takeoff and landing performance for a jet STOL transport configuration with full-span, externally blown, triple-slotted flaps
1973-10-01
Sonstige
Keine Angabe
Englisch
Externally blown flaps, aerodynamic feasibility study of a STOL-transporter
Emerald Group Publishing | 1971
|Air Force STOL Tactical Aircraft Investigation: Evaluation of Externally Blown Flaps
SAE Technical Papers | 1973
|Blown Flaps for Stol Operation
Emerald Group Publishing | 1959
|