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Numerical Simulation of Transpiration Cooling in a Laminar Hypersonic Boundary Layer (2022)

First Author: Ifti H

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.a35325

Publication URI: http://dx.doi.org/10.2514/1.a35325

Type: Journal Article/Review

Parent Publication: Journal of Spacecraft and Rockets

Issue: 5