Analytical Study of Takeoff and Landing Performance for a Jet STOL Transport Configuration with Full-Span, Externally Blown, Triple-Slotted Flaps. Technical Report NASA Technical Note TN D-7441, Research Engineering, NASA Dryden Flight Research Center

Washington, Harold P. and Gibbons, John T. (1973) Analytical Study of Takeoff and Landing Performance for a Jet STOL Transport Configuration with Full-Span, Externally Blown, Triple-Slotted Flaps. Technical Report NASA Technical Note TN D-7441, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

Takeoff and landing performance characteristics and field length requirements were determined analytically for a jet STOL transport configuration with full-span, externally blown, triple-slotted 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 various parameters (i.e., wing loading, thrust-to-weight ratio, weight, ambient temperature, altitude) on takeoff and landing field length requirements are discussed.

EPrint Type:	Other
Keywords:	Takeoff and landing, Jet STOL aircraft, Externally blown flaps
Subjects:	(01 - 09) Aeronautics: (05) Aircraft Design, Testing And Performance
ID Code:	741
Deposited On:	22 Febuary 2006
Additional Information:	49 pages.