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THREE-DIMENSIONAL SUPERSONIC FLUTTER MODEL TESTS NEAR MACH NUMBER 1.5. PART 2. EXPERIMENTAL AND THEORETICAL DATA FOR BARE WINGS AND WINGS WITH TIP TANKS
MASSACHUSETTS INST OF TECH CAMBRIDGE AEROELASTIC AND STRUCTURES RESEARCH LAB
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Three-dimensional supersonic flutter tests were made on over 75 semi-span models in the MIT blowdown wind tunnel facility. The testing technique involved injecting the model into a stable region of flow and decreasing the Mach number until instability occurred.
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