Boundary Layer Transition Measurements on Sharp and Blunt Cones in the T4 Stalker Tube
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-91017-8_142
Reference16 articles.
1. S.P. Schneider, Hypersonic laminar-turbulent transition on circular cones and scramjet Forebodies. Prog. Aerosp. Sci. 40(1–2), 1–50 (2004)
2. K.Y. Lau, Hypersonic boundary-layer transition: Application to high-speed vehicle design. J. Spacecr. Rocket. 45(2), 176–183 (2008)
3. S. Frauholz, B.U. Reinartz, S. Müller, M. Behr, Transition prediction for scramjets using γ-Reθt model coupled to two turbulence models. J. Propuls. Power 31(5), 1404–1422 (2015)
4. R.J. Stalker, R.G. Morgan, Free piston shock tunnel T4 – Initial operation and preliminary calibration, CR 181721, NASA, 1988
5. Jacobs, P. A., Morgan, R. G., Stalker, R. J., and Mee, D. J., Use of argon-helium driver-gas mixtures in the T4 shock tunnel, shock waves @ Marseille, Proceedings of the 19th International Symposium on Shock Waves, ed. by R. Brun and L. Dumitrescu, Springer, Berlin, 1993, pp. 263–268
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