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. (Author)
Analytical Study of Takeoff and Landing Performance for a Jet STOL Transport Configuration with Full-Span, Externally Blown, Triple-Slotted Flaps
1973
49 pages
Report
No indication
English
Externally blown flaps, aerodynamic feasibility study of a STOL-transporter
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