Unsteady compressible second-order boundary layers at the stagnation point of two-dimensional and axisymmetric bodies
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF01002418.pdf
Reference26 articles.
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3. Rott, N.; Lenard, M.: Vorticity effect on the stagnation-point flow of a viscous incompressible fluid. J. Aerospace Sci. 26 (1959) 542–543
4. Van Dyke, M.: Higher approximations in boundary layer theory, Part 1 and 2. J. Fluid Mech. 14 (1962) 161–177, 481–495
5. Van Dyke, M.: Second-order compressible boundary layer theory with application to blunt bodies in hypersonic flow. Hypersonic Flow Res. 7 (1962) 37–76
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