Technical notes. 3044. Effect of rapid blade-pitch increase on thrust and induced-velocity response of full scale helicopter rotor [with list of references]; by Paul J. Carpenter and Bernard Fridovich.
Publication Title:
Effect of rapid blade-pitch increase on thrust and induced-velocity response of full scale helicopter rotor [with list of references]; by Paul J. Carpenter and Bernard Fridovich.
Display Title:
Technical notes. 3044. Effect of rapid blade-pitch increase on thrust and induced-velocity response of full scale helicopter rotor [with list of references]; by Paul J. Carpenter and Bernard Fridovich.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Carpenter, Paul J. and Fridovich, Bernard
Date:
Nov. 1953
Publish Date ISO Format:
1953-11-01T00:00:00Z
Publication Start:
19531101
Publication End:
19531130
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
2
Publication year:
1953
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 26 p.+[2] leaves, il. 4°
Notes:
[Processed. The pages in brackets in each collation consist of detachable card catalog entries.]
Notes:
[Processed. The pages in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.