Gas Injection into Second Mode Instability on a 7 degree Cone at Mach 7 (2022)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/6.2022-3856
Publication URI: http://dx.doi.org/10.2514/6.2022-3856
Type: Conference/Paper/Proceeding/Abstract