Flutter (aircraft). Tests of wind tunnel flutter model, phase 1, Critical flutter speed as function of control surface dynamic balance and natural frequencies of vibration, Aircraft Branch report [with list of references; prepared by Benjamin Smilg].
Publication Title:
Flutter (aircraft). Tests of wind tunnel flutter model, phase 1, Critical flutter speed as function of control surface dynamic balance and natural frequencies of vibration, Aircraft Branch report [with list of references; prepared by Benjamin Smilg].
Display Title:
Flutter (aircraft). Tests of wind tunnel flutter model, phase 1, Critical flutter speed as function of control surface dynamic balance and natural frequencies of vibration, Aircraft Branch report [with list of references; prepared by Benjamin Smilg].
Corporate Agency Authors:
Matériel Division, Air Corps, and War Department
Sort Author:
Matériel Division
Date:
1940
Publish Date ISO Format:
1940-01-01T00:00:00Z
Publication Start:
19400101
Publication End:
19401231
Corporate/Agency Author:
Matériel Division
Publication month:
13
Publication year:
1940
SuDoc number:
W 87.11/2:8/714
Description:
ii+30 p. il. 4°
Notes:
(Air Corps. Air Corps information circular, v. 8, no. 714, Oct. 15, 1939.) [Issued with perforations.]
Notes:
(Air Corps. Air Corps information circular, v. 8, no. 714, Oct. 15, 1939.) [Issued with perforations.] ‡ Official Use. Not Available.