Reports and Memoranda - Aeronautical Research Council, Issues 3781-3800

Front Cover
H.M. Stationery Office, 1976 - Aeronautics
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Contents

A Single Kinked Swept Source Line in the Presence of a Circular Cylindrical Fuselage
4
A Single Kinked Swept Vortex in the Presence of a Circular Cylindrical Fuselage
10
Design of a Wing with Given Load Distribution when Attached to a Circular Cylindrical Fuselage
20

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