Model with unswept wing and high disk loading fan mounted in fuselage duct was tested in wind tunnel; results were used to study transition flight characteristics associated with submerged fan concept; fan produced large pitching moment variation with increasing forward speed; programming required use of wing flaps, variable angle of attack, and direct propulsive thrust.
Aerodynamics of fan-in-fuselage model
NASA -- Tech Note
1961
14 pages
Article (Journal)
English
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Engineering Index Backfile | 1942
|TIBKAT | 1942
|NTIS | 1942
|NTRS | 1942
|AERODYNAMICS OF A FAN-IN-FUSELAGE MODEL
NTRS | 1960
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