Publication:
The Effect of Stagnation Temperature and Molecular Weight Variation on Gaseous Injection Into A Supersonic Stream.

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Authors
Chrans, Larry "J"
Subjects
Advisors
Collins, Daniel J.
Date of Issue
1968-09
Date
1968-09
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
The purpose of the study was to investigate the effect of injectant stagnation temperature and molecular weight variation on the flow field generated from secondary injection of a gas normal to a supersonic stream. Experiments were conducted at a primary stream Mach number of 2.80 in a supersonic wind tunnel. Experimental data have been correlated with various theories, showing both agreement and disagreement. Data presented include penetration of secondary jet into primary flow and shock shape as correlated with the second order blast wave theory.
Type
Thesis
Description
Series/Report No
Department
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
77 p.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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