Investigation at NACA Lewis Laboratory to study variations of external pressure distributions and wave drags with fineness ratio, Mach number, and area ratio; results intended to serve as guide in design of external contours for supersonic nose inlets and to provide basis for estimating wave drag to be expected from inlets.
Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies
Nat Advisory Committee Aeronautics -- Tech Note
1950
35 pages
Charts
Report
Englisch
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Theoretical pressure distributions and wave drags for conical boattails
Engineering Index Backfile | 1953
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