Technical notes. 2483. Effects of fuselage and tail surfaces on low-speed yawing characteristics of swept-wing model as determined in curved-flow test section of Langley stability tunnel [with list of references]; by John D. Bird, Byron M. Jaquet, and John W. Cowan.
Publication Title:
Effects of fuselage and tail surfaces on low-speed yawing characteristics of swept-wing model as determined in curved-flow test section of Langley stability tunnel [with list of references]; by John D. Bird, Byron M. Jaquet, and John W. Cowan.
Display Title:
Technical notes. 2483. Effects of fuselage and tail surfaces on low-speed yawing characteristics of swept-wing model as determined in curved-flow test section of Langley stability tunnel [with list of references]; by John D. Bird, Byron M. Jaquet, and John W. Cowan.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Bird, John D., Jaquet, Byron M., and Cowan, John W.
Date:
Oct. 1951
Publish Date ISO Format:
1951-10-01T00:00:00Z
Publication Start:
19511001
Publication End:
19511031
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
3
Publication year:
1951
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 19+[8] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.