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Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 3. Wing Section and Total Surface Aerodynamic Coefficients.

M. E. Manro, Johan P. Moulijn, James D. Knittel

Abstract

This report presents the results of wind tunnel pressure distribution measurements made on a model of the Boeing supersonic transport configuration during design of the prototype airplanes. This volume contains integrated section and total surface characteristics for the wing.

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Available abstract

Key concepts: Wing, Aerodynamics, Mach number, Delta wing, Wind tunnel, Volume (thermodynamics), Supersonic speed, Wing configuration