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|Document Type: ||Report|
|Title: ||Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)|
|Authors: ||Campion, B. S.|
|Issue Date: ||Jan-1954|
|Abstract: ||The effects if distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers) are considered on a quasi-static basis. The method employed is based on the theory of Gates and Lyon but involves some extension of this theory.|
|Appears in Collections:||College of Aeronautics Reports|
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