Magnetic hypersonic rarefied flow at the stagnation point of a blunt body with slip and mass transfer
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference20 articles.
1. On reducing aerodynamic heat transfer rates by magnetohydrodynamic techniques;Meyer;J. Aerospace Sci,1958
2. On a class of compressible laminar boundary layers with pressure gradient for an electrically conducting fluid in the presence of a magnetic field;Lykoudis,1958
3. The stagnation point boundary layer in the presence of an applied magnetic field;Bush;J. Aerospace Sci,1961
4. Compressible axially symmetric laminar boundary layer flow in the stagnation region of a blunt body in the presence of magnetic field;Nath;Acta Mech,1971
5. Magnetic hypersonic flow near the stag-nation point at low Reynolds number;Chen;J. Spacecraft Rockets,1969
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Unsteady compressible boundary layer flow in the stagnation region of a sphere with a magnetic field;Archive of Applied Mechanics (Ingenieur Archiv);1997-10-23
2. Unsteady laminar compressible boundary layers with vectored mass transfer and an applied magnetic field;International Journal of Engineering Science;1992-01
3. Compressible MHD boundary layer in the stagnation region of a sphere;International Journal of Engineering Science;1990-01
4. Hypersonic stagnation-point boundary layers with massive blowing in the presence of a magnetic field;Physics of Fluids;1979
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