Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 3.67

Edward W. Perkins, Leland H. Jorgensen
naca-rm-a52h28
Nov 1952

Foredrag measurements have been made at zero angle of attack for a series of fineness ratio 3 nose shapes. The models included various theoretically derived minimum drag shapes, hemispherically blunted cones, and other more common profiles.

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