Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor
Author:
Funder
Agency for Defense Development
Pusan National University
Defense Acquisition Program Administration
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference18 articles.
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3. Experimental and numerical investigations of freejet and direct-connect dual-mode scramjet;Xiao;Aerosp. Sci. Technol.,2018
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