Requirements for simulating flight conditions relevant to flutter and their application to transonic and supersonic flight; it is shown that tests are conveniently carried out in tunnel with constant stagnation temperature but adjustable Mach number and stagnation pressure; application of similarity requirement to investigation to determine transonic flutter characteristics of tail unit of specific aircraft. (Received Mar 1960)
Flutter investigations in high-speed wind tunnels
AGARD -- Report
AGARD -- Reports ; n 222
1958
37 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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