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Experimental Studies of Hypersonic Shock Impingement on a Transpiration-Cooled Flat Plate (2023)

First Author: Naved I

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/10.2514/1.a35416

Publication URI: http://dx.doi.org/10.2514/1.a35416

Type: Journal Article/Review

Parent Publication: Journal of Spacecraft and Rockets

Issue: 3