A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds
Description:
An approximate method is presented for the calculation of the external lift, moment, and pressure drag of slender open-nose bodies of revolution of supersonic speeds. The lift, moment, and pressure drag of a typical ram-jet body shape are calculated at Mach numbers 1.45, 1.60, 1.75, and 3.00; and the lift and moment results are compared with available experimental data. The agreement of the calculated lift and moment data with the experimental data is excellent. The pressure-drag comparison was…
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Date:
December 29, 1945
Creator:
Brown, Clinton E. & Parker, Hermon M.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department