A rapid graphical method for computing the pressure distribution at supersonic speeds on a slender arbitrary body of revolution

Jim Rogers Thompson
naca-tn-1768
Jan 1949


A method is presented by which the pressure distribution on a slender, arbitrary body of revolution moving at supersonic speeds at zero angle of attack may be calculated with an appreciable saving of time as compared with that required by other methods.

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http://naca.central.cranfield.ac.uk/reports/1949/naca-tn-1768.pdf