Heat Transfer Measurements of a Transpiration-Cooled Stagnation Point in Transient Hypersonic Flow (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.t6610

Publication URI: http://dx.doi.org/10.2514/1.t6610

Type: Journal Article/Review

Parent Publication: Journal of Thermophysics and Heat Transfer

Issue: 2