Approximate theory of buffeting is presented, based on assumption of harmonic disturbing forces; two cases of buffeting considered: namely, for tail angle of attack greater and less than stalling angle, respectively; analysis of nature of forced vibrations, possible load limits on tail, and methods of elimination of buffeting. Bibliography. English translation of Report No. 395, of Central Aero-Hydrodynamical Inst, Moscow, 1939.
Tail buffeting
Nat Advisory Committee Aeronautics -- Tech Memo
1943
39 pages
11 Supp sheets
Report
English
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