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Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X

   
 
 

 

Laminar boundary layer at a discontinuity in wall curvature


Authors: A. F. Messiter and J. J. Hu
Journal: Quart. Appl. Math. 33 (1975), 175-181
MSC: Primary 76.41
DOI: https://doi.org/10.1090/qam/446071
MathSciNet review: 446071
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Abstract: The discontinuity in pressure gradient predicted for two-dimensional inviscid subsonic or supersonic flow at a jump discontinuity in wall curvature is smoothed by means of local solutions which take into account the interaction of a laminar boundary layer with the external flow.


References [Enhancements On Off] (What's this?)

    K. Stewartson and P. G. Williams, Self-induced separation, Proc. Roy. Soc. London Ser. A 312 181–206 (1969) K. Stewartson, On the flow near the trailing edge of a flat plate. II, Mathematika 16, 106–121 (1969) A. F. Messiter, Boundary-layer flow near the trailing edge of a flat plate, SIAM J. Appl. Math. 18, 241–257 (1970) K. Stewartson, On laminar boundary layers near corners, Q. J. Mech. Appl. Math. 23, 137–152 (1970); corrections and an addition, 24, 387–389 (1971) H. M. Brilliant and T. C. Adamson, Jr., Shock wave-boundary layer interactions in laminar transonic flow, AIAA J. 12, 323–329 (1974).
  • W. G. L. Sutton, On the equation of diffusion in a turbulent medium, Proc. Roy. Soc. London Ser. A 182 (1943), 48–75. MR 8880, DOI https://doi.org/10.1098/rspa.1943.0023

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Article copyright: © Copyright 1975 American Mathematical Society