Julian H. Allen
naca-tn-2044
Mar 1950
In connection with a study of the flow around slender inclined bodies of revolution, a simplified solution for the pressure distribution on such a body has been developed. The solution should be suitable for bodies of high fineness ratio even at low supersonic speeds, provided the angle of attack is small.
An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2044.pdf