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FREE-FLIGHT TESTS OF 45 DEG SWEPT WINGS OF ASPECT RATIO 3.15 AND TAPER RATIO 0.54 TO MEASURE WING DAMPING OF THE FIRST BENDING MODE AND TO INVESTIGATE THE POSSIBILITY OF FLUTTER AT TRANSONIC SPEEDS

Burke R O'Kelly, R. R. Lundstrom, William T Lauten

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Abstract

Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter

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Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter

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Available abstract

Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter

Key concepts: Wing, Aspect ratio (aeronautics), Measure (data warehouse), Bending, Structural engineering, Swept wing, Materials science, Engineering

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FREE-FLIGHT TESTS OF 45 DEG SWEPT WINGS OF ASPECT RATIO 3.15 AND TAPER RATIO 0.54 TO MEASURE WING DAMPING OF THE FIRST BENDING MODE AND TO INVESTIGATE THE POSSIBILITY OF FLUTTER AT TRANSONIC SPEEDS — Research Paper | ScholarLens