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Development of a Supersonic Nozzle and Test Section for use with a Magnetic Suspension System for Re-Entry Aeroshell Models

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1. http://rave.ohiolink.edu/etdc/view?acc_num=case1544179612537658

Identifer	oai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:case1544179612537658
Date	29 January 2019
Creators	Chen, Ru-Ching
Publisher	Case Western Reserve University School of Graduate Studies / OhioLINK
Source Sets	Ohiolink ETDs
Language	English
Detected Language	English
Type	text
Source	http://rave.ohiolink.edu/etdc/view?acc_num=case1544179612537658
Rights	unrestricted, This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.