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Experimental research on stability and transition in high-speed wakes. Part 2. Influence of parameters of supersonic free flow on development of disturbances in a wake

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Języki publikacji
EN
Abstrakty
Rocznik
Strony
251--260
Opis fizyczny
Bibliogr. 19 poz., wykr.
Twórcy
Bibliografia
  • 1. G.I. BAGAEV, V.A. LEBIGA, V.G. PRIDANOV, V.V. CHERNYH, A supersonic wind tunnel T-325 wiłh low-degree turbulence [in Russian], [in:] Aerodynamic Researches, 11-13, Novo-sibirsk 1972.
  • 2. T.L. JACKSON, CE. GROSCH, Inmscid spatial stability of a compressible mizing layer, NASA-CR-181671, ICASE Rep. no.2, 1988.
  • 3. T.L. JACKSON, CE. GROSCH, Inviscid spatial stability of a compressible mixing layer, J. Fluid Mech., 208, 609-637, 1989.
  • 4. T.L. JACKSON, CE. GROSCH, Absolute/convective instabilities and the convective Mach number in a compressible mixing layer, Phys.Fluids A, 2, 6, 949-954, 1990.
  • 5. T.L. JACKSON, CE. GROSCH, Inmscid spatial stability of a compressible mixing layer. Part 2. The flame sheet model, J. Fluid Mech., 217, 391-420, 1990.
  • 6. T.L. JACKSON, CE. GROSCH, Inmscid spatial stability of a compressible mixing layer. Part 3. Effect of thermodynamics, J. Fluid Mech., 224, 159-175, 1991.
  • 7. A.N. KUDRYAVTSEV, A.S. SOLOVYOV, Stability of a shear layer of compressible gas [in Rus-sian], Zh. Prikl. Mekh. Tekh. Fiz., 6, 119-127, 1989.
  • 8. A.N. KUDRYAVTSEV, A.S. SOLOVYOV, Stability of a mscous compressible shear layer with temperature leap [in Russian], Zh. Prikl.Mekh. Tekh. Fiz., 4, 88-95, 1991.
  • 9. S.A. RAGAB, J.L. WU, Linear instabilities in two-dimensional compressible mixing layers, Phys. Fluids A, 1, 957-966, 1989.
  • 10. M. ZHUANG, T. KUBOTA, P.E. DIMOTAKIS, Instability of in viscid, compressible free shear layers, AIAA J., 28, 10, 1728-1733, 1990.
  • 11. S. KIM, A new mixing length model for supersonic shear layers, AIAA Pap., 18, 6p., 1990.
  • 12. M.G. MACARAEG, CL. STREETT, New instability modes for bounded, free shear flows, Phys. Fluids A, 1, 8, 1305-1307, 1989.
  • 13. L. LEES, Hypersonic wakes and trails, AIAA J., 2, 3, 417-428, 1964.
  • 14. L. LEES, H. GOLD, Stability of laminar boundary layers and wakes at hypersonic speeds. Part 1. Stability of laminar wakes, [in:] Fund. Phenom. in Hypersonic Flow, 4, 310-337, Cornell Univ. Press, Buffalo, N.Y. 1964.
  • 15. S. YA, GERTSENSTEIN, A.V. KOSHKO, Stability of axis-symmetrical compressible in viscid wake [in Russian], [in:] Aerodynamics of large speeds, 142-150, Institute of the Mechanics of Moscow Univ., Moscow 1972.
  • 16. J.H. CHEN, B.J. CANTWELL, N.N. MANSOUR, The effect of Mach number on the stability of a plane supersonic wake, Phys. Fluids A, 2, 6, 984-1004, 1990.
  • 17. D.K. MCLAUGHLIN, Experimental investigation of the stability of the laminar supersonic cone wake, AIAA J., 9, 4, 696-702, 1971.
  • 18. W. BEHRENS, Far wake behind cylinders at hypersonic speeds: II. Stability, AIAA J., 6, 2, 225-232, 1968.
  • 19. A. DEMETRIADES, Hot-wire measurements in the hypersonic wakes of slender bodies, AIAA J., 2, 2, 245-250, 1964.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPB2-0063-0007
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