Spin (aircraft). Effect of horizontal-tail position on hinge moments of unbalanced rudder in attitudes simulating spin conditions [with list of references]; by Ralph W. Stone, jr., and Sanger M. Burk, jr.
Publication Title:
Spin (aircraft). Effect of horizontal-tail position on hinge moments of unbalanced rudder in attitudes simulating spin conditions [with list of references]; by Ralph W. Stone, jr., and Sanger M. Burk, jr.
Display Title:
Spin (aircraft). Effect of horizontal-tail position on hinge moments of unbalanced rudder in attitudes simulating spin conditions [with list of references]; by Ralph W. Stone, jr., and Sanger M. Burk, jr.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Stone, Ralph W. jr. and Burk, Sanger M. jr.
Date:
June 1947
Publish Date ISO Format:
1947-06-01T00:00:00Z
Publication Start:
19470601
Publication End:
19470630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1947
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/1337
Description:
cover title, 13 p. 16 pl. 34 p. of pl. 4°
Notes:
(Technical note 1337.) [Processed.]
Notes:
(Technical note 1337.) [Processed.] † Distribution Made by Issuing Office.