1972•Defense Technical Information Center (DTIC)Requires access
Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 9. Horizontal Stabilzer Section and Total Surface Aerodynamic Coefficients, Chordwise Pressure Distributions.
M. E. Manro, Johan P. Moulijn, James D. Knittel
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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 and local surface chordwise pressure distributions for the horizontal stabilzer.