Correction: Performance of Transpiration-Cooled Heat Shields for Reentry Vehicles (2020)

First Author: Hermann T
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.j058515.c1

Publication URI: http://dx.doi.org/10.2514/1.j058515.c1

Type: Journal Article/Review

Parent Publication: AIAA Journal

Issue: 11