The possibility of simulating in wind tunnels the parameters of hypersonic flow and the conditions in the combustor of hypersonic scramjet engine
V. I. Alfyorov, L. M. Dmitriev, B. V. Egorov, Yu. E. Markachev, A. P. Rudakova

This publication is cited in the following articles:

1. V A Bityurin, A N Bocharov, S S Bychkov, T N Kuznetsova, N V Tretyakova, N I Batura, N G Zhurkin, “Measurement of heat flux to model surface in the wind tunnel SMGDU”, J. Phys.: Conf. Ser., 1112 (2018), 012001