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Contributions of wing, tail, and fuselage to the aerodynamic characteristics of a semispan model of a supersonic airplane configuration at transonic speeds from tests by the NACA wing-flow method

Investigation of the Distribution of Lift, Drag, and Pitching Moment Between the Wing and Fuselage of a 1/30-Scale Semispan Model of the Bell X-5 Airplane at a Mach Number of 1.24 by the NACA Wing-Flow Method

Landing conditions for large airplanes in routine operations

Published Year

• 1950-1959 (3) *

Subject

• Airplanes--Landing (1)

Author

• Silsby, Norman S. (3) *
• Harrin, Ezlaslav N. (1)

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