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 10. Horizontal Stabilizer Net Chordwise Pressure Distributions and Isobars.
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 horizontal stabilizer net chordwise pressure distributions and isobars showing the effect of angle of attack, stabilizer deflection and elevator deflection.