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- W3037386744 abstract "Wind-tunnel tests of the T-tail of a wide-body jet airplane were made at Mach numbers up to 1.02. The model consisted of a 1/13-size scaled version of the T-tail, fuselage, and inboard wing of the airplane. Two interchangeable T-tails were tested, one with design stiffness for flutter-clearance studies and one with reduced stiffness for flutter-trend studies. Transonic antisymmetric-flutter boundaries were determined for the models with variations in: (1) fin-spar stiffness, (2) stabilizer dihedral angle (-5 deg and 0 deg), (3) wing and forward-fuselage shape, and (4) nose shape of the fin-stabilizer juncture. A transonic symmetric-flutter boundary and flutter trends were established for variations in stabilizer pitch stiffness. Photographs of the test configurations are shown." @default.
- W3037386744 created "2020-07-02" @default.
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- W3037386744 date "1975-12-01" @default.
- W3037386744 modified "2023-09-29" @default.
- W3037386744 title "Experimental parametric studies of transonic T-tail flutter" @default.
- W3037386744 hasPublicationYear "1975" @default.
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