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Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)
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Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)

College of Aeronautics

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Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers) by College of Aeronautics. Published by College of Aeronautics in 1954. Publication and catalogue information, links to buy online and reader comments.

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