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.
Year: 1953
Document Type: MAIN
SUDOC: Y 3.N21/5:15/L53J09a
Series: NACA research memorandum ;
Report Number: L53J09a
Subject: Airplanes--Wings, Swept-back
Link: https://hdl.handle.net/2027/mdp.39015095100734

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