Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed

Publisher Website

8 July 2007

conference paper
conference paper
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.2007-5066

Abstract

No abstract available

Cited by 14 articles