Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45° sweptback-wing--body combination, by Harold S. Johnson et al.

Title:	Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45° sweptback-wing--body combination
Author:	Johnson, Harold S.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Advisory Committee for Aeronautics
Note:	Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953

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Subject:	Airplanes -- Wings, Swept-back
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