Experimental Study of Heat Flux in the Pseudo-shock Region
Author:
Affiliation:
1. The Research and Development Directorate, JAXA
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/59/5/59_T-15-76/_pdf
Reference8 articles.
1. 1) Matsuo, K., Miyazato, Y., and Kim, H.-D.: Shock Train and Pseudo-Shock Phenomena in Internal Gas Flows, Progr. Aerospace Sci., 35 (1999), pp. 33–100.
2. 2) Back, L. H., Cuffel, R. F., and Massier, P. F.: Flow and Heat Transfer Measurements along a Cooled Supersonic Diffuser, AIAA J., 22 (1984), pp. 777–780.
3. 3) Zaikovskii, V. N., Trofimov, V. M., and Shtrekalkin, S. I.: Experimental and Computational Investigation of Heat Fluxes in a Supersonic Diffuser, J. Appl. Mech. Tech. Phys., 37 (1996), pp. 135–140.
4. 4) Back, L. H. and Cuffel, R. F.: Changes in Heat Transfer from Turbulent Boundary Layers Interacting with Shock Waves and Expansion Waves, AIAA J., 8 (1970), pp. 1871–1873.
5. 5) Cuffel, R. F. and Back, L. H.: Flow and Heat Transfer Measurements in a Pseudo-Shock Region with Surface Cooling, AIAA J., 14 (1976), pp. 1716–1722.
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