Data presented through Mach number range from 0.60 to 1.18 and Reynolds number from 2.3 to 5.5 million; results obtained by forced oscillation technique in which electrohydraulic servo valve was used to power drive system.
Experimental wind-tunnel investigation of transonic damping-in-pitch characteristics of two wing-body combinations
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 11-30-58A
1958
26 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Transonic Wind Tunnel Test of Wing Oscillating in Pitch
AIAA | 2018
|Wind-tunnel wall corrections for wing-body combinations
Engineering Index Backfile | 1949
|Transonic flow about lifting wing-body combinations
NTRS | 1974
|Transonic flow about lifting wing-body combinations
AIAA | 1974
|