Model of hypothetical canard airplane, designed to be of same size and general aerodynamic characteristics as Boeing B-247 airplane, was tested in NACA gust tunnel at one wind loading, one forward speed, one gust velocity, and three gust gradients; results of tests presented and discussed.
Measurements and analysis of motion of canard airplane model in gusts
Nat Advisory Committee Aeronautics -- Tech Note
1940
20 pages
9 Supp Sheets, Bibliography
Aufsatz (Zeitschrift)
Englisch
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Canard type light personal airplane
Engineering Index Backfile | 1946
|Canard type light personal airplane
Engineering Index Backfile | 1946
|Theory of an airplane encountering gusts II
NTRS | 1918
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