A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum., by Emma Jean Landrum et al.

Title:	A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum.
Author:	Landrum, Emma Jean
Author:	United States. National Aeronautics and Space Administration
Note:	National Aeronautics and Space Administration :, 1962

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Subject:	Aerodynamics, aircraft
Subject:	Aerodynamics, missiles and space vehicles
Subject:	Aircraft
Subject:	Airplanes -- Wings, Swept-back -- Design and construction
Subject:	Airplanes -- Wings, Swept-back -- Mathematical models
Subject:	Camber (Aerofoils)
Subject:	Stability and control
Subject:	Stresses and loads
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