Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. [Part] 2, Isentropic-spike all-external compression inlet, by L. J. Obery et al.

Title:	Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. [Part] 2, Isentropic-spike all-external compression inlet
Author:	Obery, L. J.
Author:	Englert, G. W.
Author:	United States. National Advisory Committee for Aeronautics
Author:	Lewis Flight Propulsion Laboratory
Note:	National Advisory Committee for Aeronautics, 1951

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Subject:	Aerodynamics, Supersonic
Subject:	Aeronautics -- Research
Subject:	Air ducts
Subject:	Air flow
Subject:	Charts, diagrams, etc.
Subject:	Diffusers
Subject:	Noses (Aircraft)
Subject:	Wind tunnel testing
Other copies:	Look for editions of this book at your library, or elsewhere.