Influence of flow conditions over the forebody of a hypersonic air inlet on the flow of air in a boundary-layer bleed channel
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
http://link.springer.com/content/pdf/10.1134/S0869864319050020.pdf
Reference25 articles.
1. K.R. Jackson, M.R. Gruber, and S. Buccellato, Mach 6–8+ hydrocarbon-fueled scramjet flight experiment: the HIFiRE flight 2 project, J. Propulsion and Power, 2015, Vol. 31, No. 1 P. 36–53.
2. D. Herrmann and A. Gulhan, Experimental analysis of inlet characteristics of an air-breathing missile with boundary-layer bleed, J. Propulsion and Power, 2015, Vol. 31, No. 1 P. 170–179.
3. Yu.P. Goonko and I.I. Mazhul, Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression, Thermophysics and Aeromechanics, 2015, Vol. 22, No. 5 P. 545–559.
4. Yu.P. Goonko and I.I. Mazhul, On the question of starting frontal axisymmetric inlets tested in hot-shot wind tunnels, Thermophysics and Aeromechanics, 2017, Vol. 24, No. 3 P. 369–381.
5. D.M. Van Wie, Scramjet inlets, scramjet propulsion, Progress in Astronautics and Aeronautics, 2000, Vol. 189, Res. VA, AIAA, P. 447–511.
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