The effect of blast wave incidence angle on hypersonic shock-on-shock interaction.

A previous theoretical study of weak blast wave impingement on slender hypersonic wedges for the case of head-on incidence is herein extended to include the effect of oblique incidence. Assuming linearized small perturbations from the original steady wedge flow, we obtain an analytical solution for...

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Bibliographic Details
Corporate Author: Aerospace Corporation. Laboratory Operations
Other Authors: Inger, George R.
Format: Government Document Book
Language:English
Published: Ft. Belvoir : Defense Technical Information Center, March 1966.
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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: D 301.71:66-62
D 301.71:66-62 Available Place a Hold