Flutter Investigation on the High Subsonic and Transonic Speed Range on Cantilever Delta-Wing Plan Forms With Leading-Edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees
Description:
Report presenting results of flutter testing on three cantilever delta-wing plan forms at a range of Mach numbers. The time and location of flutter and results of the flutter calculations are provided for each of the wings.
Date:
January 31, 1957
Creator:
Lauten, William T., Jr. & Burgess, Marvin F.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department