9 citations to 10.1007/BF02031768 (Crossref Cited-By Service)

1. M. V. Silnikov, M. V. Chernyshov, “Supersonic flow gradients at an overexpanded nozzle lip”, Shock Waves, 28, № 4, 2018, 765  
2. Mihail Chernyshov, Alexandr Tyapko, A. Borodinecs, V. Sergeev, N. Vatin, “Optimal triple configurations of stationary shocks”, MATEC Web Conf., 245, 2018, 12006  
3. M. V. Chernyshov, “Extreme Triple Configurations with Negative Slope Angle of the Reflected Shock”, Russ. Aeronaut., 62, № 2, 2019, 259  
4. Mikhail V. Silnikov, Mikhail V. Chernyshov, “Incident shock strength evolution in overexpanded jet flow out of rocket nozzle”, Acta Astronautica, 135, 2017, 172  
5. M. V. Silnikov, M. V. Chernyshov, Shock Wave Interactions, 2018, 57  
6. V. N. Uskov, M. V. Chernyshov, “Extreme shockwave systems in problems of external supersonic aerodynamics”, Thermophys. Aeromech., 21, № 1, 2014, 15  
7. M.V. Chernyshov, O.A. Tolpegin, “Optimal regular reflection of oblique shocks”, Acta Astronautica, 163, 2019, 225  
8. M. V. Chernyshov, L. G. Gvozdeva, “Triple Configurations of Steady and Propagating Shocks”, Russ. Aeronaut., 65, № 2, 2022, 319  
9. M.V. Chernyshov, K.E. Savelova, “EXTREME TRANSLATIONAL IMPACT OF TRIPLE-SHOCK CONFIGURATIONS OF BLAST WAVES IN A CONFINED VOLUME OF AN ORBITAL STATION”, Acta Astronautica, 2024