Author:
Levin V. A.,Afonina N. E.,Gromov V. G.,Smekhov G. D.,Khmelevsky A. N.,Markov V. V.
Subject
Nuclear and High Energy Physics,Radiation
Reference14 articles.
1. A.N. Kraiko and N.I. Tillyayeva, Countoring spike nozzles and determining the optimal direction of their primary flows, Fluid Dynamics, 2007, Vol. 42, No. 2, P. 321–329.
2. A.P. Vasiliev, V.M. Kudryavtsev, and V.A. Kuznetsov, Fundamentals of Rocket Engine Theory and Calculations, Vysshaya Shkola, Moscow, 1993.
3. D.H. Huang, Aerospike engine technology demonstration for space propulsion, AIAA Paper No. 74-1080. (AIAA/SAE 10th Propulsion Conf. 21–23 October 1974, San Diego, California).
4. T.-S. Wang, Analysis of linear aerospike plume-induced X-33 base-heating environment, J. Spacecraft Rockets, 1999, Vol. 36, No. 6, P. 777–783.
5. V.A. Levin, V.N. Perezhogin, and A.N. Khmelevsky, Features of combustion product flow structure in a spherical semi-open cavity, Combustion, Explosion and Shock Waves, 1995, Vol. 31, No. 1, P. 30–36.
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献