Damping in Pitch of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds
Description:
Memorandum presenting the application of the concept of indicial functions to the analysis of the aerodynamic phenomena associated with the short-period pitching mode of wings in subsonic and supersonic flight. Simple physical relationships are pointed out and are used to study the effect on the rotary-damping-moment coefficient of changes in center-of-gravity position, Mach number, aspect ratio, plan form, frequency, and thickness.
Date:
April 8, 1953
Creator:
Tobak, Murray
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department