Airplane under consideration is high aspect ratio, transonic bomber from which turbojet engines are suspended in nacelles below wings; chief difficulties were in accurately predicting wing torsional frequencies and in adequately representing nacelle pylon characteristics; adequate analysis is possible when these are properly taken into account.
Comparison of experimental and analytical flutter characteristics for swept wing jet bomber
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1954 Flutter
1954
24 pages
Aufsatz (Konferenz)
Englisch
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A COMPARISON OF EXPERIMENTAL AND ANALYTICAL FLUTTER CHARACTERISTICS FOR A SWEPT WING JET BOMBER
SAE Technical Papers | 1954
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