Author:
Pinto D. Romanelli,Marcos T. V. C.,Galvão V. A. B.,Oliveira A. C.,Chanes J. B.,Minucci M. A. S.,Toro P. G. P.
Publisher
Springer Berlin Heidelberg
Reference7 articles.
1. Nagamatsu, H.T.: Shock Tube Technology and Design. In: Ferri, A. (ed.) Fundamental Data Obtained from Shock Tube Experiments, ch. III. Pergamon Press (1961)
2. Toro, P.G.P., Minucci, M.A.S., Chanes Jr., J.B., Oliveitra, A.C., Gomes, F.A.A., Myrabo, L.N., Nagamatsu, H.T.: New Hypersonic Shock Tunnel at the Laboratory of Aerothermodynamics and Hypersonics. In: Nagamatsu, H.T. (ed.) 4th International Symposium on Beamed Energy Propulsion, Hawaii (2007)
3. Minucci, M.A.S.: An Experimental Investigation of a 2-D Scramjet Inlet at Flow Mach Numbers of 8 to 25 and Stagnation Temperatures of 800 to 4100 K. Ph.D. Thesis, Rensselaer Polytechnic Institute, New York (1991)
4. Nagamatsu, H.T., Geiger, R.E., Sheer Jr., R.E.: Real Gas Effects in Flow over Blunt Bodies at Hypersonic Flow. J 27(4) (1960)
5. Nagamatsu, H.T., Workman, J.B., Sheer Jr., R.E.: Hypersonic Nozzle Expansion of Air with Atom Recombination Present. J. of the Aero/Space Sciences 28(11), 833–837 (1961)
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