Effect of favorable pressure gradients on transition for several bodies of revolution at Mach 3.12 / by John R. Jack.

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Bibliographic Details
Main Author:	Jack, John R.
Corporate Authors:	Lewis Flight Propulsion Laboratory, United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington : National Advisory Committee for Aeronautics, [1958]
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 4313.
Subjects:	Transition flow. Aerodynamics, Supersonic. Aerodynamic load. Body of revolution.

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Call Number:	Y 3.N 21/5:6/4313
Y 3.N 21/5:6/4313	Available Place a Hold