Controlled supercritical crossflow on supersonic wings - An experimental validation

Publisher Website

14 July 1980

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

https://doi.org/10.2514/6.1980-1421

Abstract

No abstract available

This publication has 3 references indexed in Scilit:

A numerical procedure for the computation of supersonic conical flows
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1978
Interactions between shock waves and turbulent boundary layers
Progress in Aerospace Sciences, 1970
THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDS
Published by Elsevier ,1962