Supersonic film cooling

Publisher Website

17 August 1990

proceedings article
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1990-5239

Abstract

No abstract available

This publication has 3 references indexed in Scilit:

Film cooling effectiveness in hypersonic turbulent flow
AIAA Journal, 1970
An experimental investigation of turbulent slot injection at Mach 6
AIAA Journal, 1970
Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.
AIAA Journal, 1966