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Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K.
Published in:
Doklady Physical Chemistry, 2018, v. 481, n. 1, p. 100, doi. 10.1134/S0012501618070035
By:
- 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.
Publication type:
Article
Continuous Detonation Combustion of Hydrogen: Results of Wind Tunnel Experiments.
Published in:
Combustion, Explosion, & Shock Waves, 2018, v. 54, n. 3, p. 357, doi. 10.1134/S0010508218030139
By:
- 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.
Publication type:
Article
Detonation waves in a reactive supersonic flow.
Published in:
Combustion, Explosion, & Shock Waves, 2006, v. 42, n. 5, p. 568, doi. 10.1007/s10573-006-0089-4
By:
- Vasil’ev, A. A.;
- Zvegintsev, V. I.;
- Nalivaichenko, D. G.
Publication type:
Article