Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K
Titel:
Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K
Auteur:
Frolov, S. M. Zvegintsev, V. I. Ivanov, V. S. Aksenov, V. S. Shamshin, I. O. Vnuchkov, D. A. Nalivaichenko, D. G. Berlin, A. A. Fomin, V. M. Shiplyuk, A. N. Yakovlev, N. N.