Experimental Flutter Results for Cantilever-Wing Models at Mach Numbers Up to 3.0
Description:
Report presenting experimental flutter testing at Mach numbers up to 3.0 using cantilever-wing models with 0 to 60 degree sweepback and 60 degree delta-wing models. The main variables explored were the high Mach number and center-of-gravity location on flutter trends. The theoretical results for flutter analyses were noted to be lower than the experimental results.
Date:
June 14, 1955
Creator:
Tuovila, W. J. & McCarty, John Locke
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department