References
Welsh, W. E., jr.: Ground test facilities for aerothermodynamic simulation of ballistic re-entry vehicles nosetip conditions. TR-1001 (2240-10)-6, May 1976, Aerospace Corp.
Mirels, H., Welsh, W. E., Jr.: Stagnation-point boundary layer with large wall-to-freestream enthalpy ratio. AIAA J.6, 1105–1111 (1968).
Gribben, R. J.: The fluctuating flow of a gas near a stagnation point on a hot wall. Trans. ASME, J. Appl. Mech.38, 820–828 (1971).
Bush, W. B.: The stagnation point boundary layer in the presence of an applied magnetic field. J. Aerospace Sci.28, 610–611 (1961).
Nath, G.: Compressible axially symmetric laminar boundary layer flow in the stagnation region of a blunt body in the presence of magnetic field. Acta Mechanica12, 267–273 (1971).
Wortman, A., Mills, A. F.: Highly accelerated compressible laminar boundary layer flows with mass transfer. Trans. ASME, J. Heat Transfer93, 281–289 (1971).
Libby, P. A., Liu, T. M.: Some similar laminar flows obtained by quasilinearization. AIAA J.6, 1541–1548 (1968).
Wu, P., Libby, P. A.: Further results on the stagnation-point boundary layer with hydrogen injection. Combustion Science and Technology6, 159–168 (1972).
Lykoudis, P. S.: Velocity overshoots in magnetic boundary layers. J. Aerospace Sci.28, 896–897 (1961).
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Muthanna, M., Nath, G. Stagnation-point boundary layer with hot wall in the presence of a magnetic field. Acta Mechanica 26, 295–299 (1977). https://doi.org/10.1007/BF01177151
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DOI: https://doi.org/10.1007/BF01177151