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Original publisher: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989] OCLC Number: (OCoLC)25291040 Subject: Fluid dynamics -- Mathematical models. Excerpt: ... surface; there must be somefluid flowing in and somefluid flowing out. All 3-D separation surfacesare a kind of vortex sheet. In general, for 3-D separation, an attachment is not the reverseof a separation, or vice versa. REFERENCES 1. Kaufman, L.G.; Korkegi, R.H.; and Morton, L.C.: Shock Impingement oCausedbyn Boundary Layer Separation Ahead of Blunt Fin. ARL 72-0118, Wright-Patters Air ForceBase, Ohio, 1972. 2. Hung, C. M.; and MacCormack, R. W.: NumericM Solution of Tllree-Dimensional Shock-Waveand Turbulent Boundary-Layer Interaction. AIAA J., vol. 16, no. 12, Dec. 1978, pp. 1090-1096. 3. Horstman, C. C.; and Hung, C. M.: Computation of 3-D Turbulent SeparatedFlow at SupersonicSpeed.AIAA Paper No. 79-0002, 1979. 4. Dolling, D.S.; andBogdonoff; S.M: Blunt Fin-Induced ShockWave / Turbulent Bound-ary Layer Interaction. AIAA J., vol. 20, no. 12, 1982, pp. 1674-1680. 5. Hung, C. M.; and Buning, P. G.: Sinmlation of Blunt-Fin-Induced Shock Wave and Turbulent Boundary-Layer Interaction. J. Fluid Mech., vol. 154, May 1985, pp. 163-185 6. Knight, D. D.; Horstman, C. C.; Shapey, B.; and Bogdonoff, S.: The Flowfield Generated by a 20 ° Structure of the 3-D ShockWave-Boundary Layer hlteraction Sharp fin at Mach 3. AIAA Paper No. 86-0343, 1986. 7. Fomison, N. R.; and Stollery, J. L.: The Effects of Sweep and Bluntness on a Glancing Shock Wave Turbulent Boundary Layer Interaction. AGARD CP 428, Paper 8, 1987. 8. Dolling, D.S.: Unsteadiness of Supersonic and Hypersonic Shock-Induced Turbu-lent Boundary Layer Separation. AGARD-FDP / VKI Special Course on " Three-Dimensional Supersonic and Hypersonic Flows Including Separation ", May 8-12, 1989. 9. Eichelbrenner, E. A.: Three-Dimensional Bound
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Computation of Navier-Stokes equations for three-dimensional flow separation
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