Numerical study of a fully confined supersonic slot impinging jet from bleed system
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. Thrust losses in hypersonic engines. Part 1: methodology;Riggins;J. Propuls. Power,2015
2. Reduction of shock induced boundary layer separation in hypersonic inlets using bleed;Schulte;Aerosp. Sci. Technol.,1998
3. Manipulation of shock/boundary-layer interactions in hypersonic inlets;Schulte;J. Propuls. Power,1999
4. Experimental investigation of a two-dimensional and a three-dimensional scramjet inlet at Mach 7;Häberle;J. Propuls. Power,2008
5. Internal flowfield investigation of a hypersonic inlet at Mach 6 with bleed;Häberle;J. Propuls. Power,2015
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