메뉴 건너뛰기




Volumn , Issue , 1996, Pages

Laminar-turbulent transition research in the purdue mach-4 quiet-flow ludwieg tube

Author keywords

[No Author keywords available]

Indexed keywords

GLOW DISCHARGES; HYPERSONIC AERODYNAMICS; NASA; PULSED LASERS;

EID: 85088358953     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2191     Document Type: Conference Paper
Times cited : (8)

References (79)
  • 3
    • 0000406298 scopus 로고
    • Aerothermodynamics and transition hi high-speed wind tunnels at NASA Langley
    • I. E. Beckwith and C. G. Miller III. Aerothermodynamics and transition hi high-speed wind tunnels at NASA Langley. Annual Review of Fluid Mechanics, 22:419-439, 1990.
    • (1990) Annual Review of Fluid Mechanics , vol.22 , pp. 419-439
    • Beckwith, I.E.1    Miller, C.G.2
  • 7
    • 84983097600 scopus 로고    scopus 로고
    • M. Y. Hussaini and R. G. Voigt, editors, Instability and Transition, Volume I, Springer-Verlag, 1990. Materials of the workshop held May 15-June 9, 1989 hi Hampton, Virginia
    • D. M. Bushnell. Notes on initial disturbance fields for the transition problem. In M. Y. Hussaini and R. G. Voigt, editors, Instability and Transition, Volume I, pages 217-232. Springer-Verlag, 1990. Materials of the workshop held May 15-June 9, 1989 hi Hampton, Virginia.
    • Notes on Initial Disturbance Fields for the Transition Problem , pp. 217-232
    • Bushnell, D.M.1
  • 8
    • 84983198426 scopus 로고
    • NASA Langley Research Center, Hampton, Virginia
    • Dennis M. Bushnell. Personal communication, 1995. NASA Langley Research Center, Hampton, Virginia.
    • (1995) Personal Communication
    • Bushnell, D.M.1
  • 9
    • 0029388588 scopus 로고
    • An instability in supersonic boundary-layer flow over a compression ramp
    • K. W. Cassel, A. I. Ruban, and J. D. A. Walker. An instability in supersonic boundary-layer flow over a compression ramp. Journal of Fluid Mechanics, 300:265-285, 1995.
    • (1995) Journal of Fluid Mechanics , vol.300 , pp. 265-285
    • Cassel, K.W.1    Ruban, A.I.2    Walker, J.D.A.3
  • 10
    • 0024673637 scopus 로고
    • Boundary-layer transition on a cone and flat plate at Mach 3. 5
    • F. -J. Chen, M. R. Malik, and I. E. Beckwith. Boundary-layer transition on a cone and flat plate at Mach 3. 5. AIAA Journal, 27(6):687-693, 1989.
    • (1989) AIAA Journal , vol.27 , Issue.6 , pp. 687-693
    • Chen, F.-J.1    Malik, M.R.2    Beckwith, I.E.3
  • 13
    • 0029193848 scopus 로고
    • Viscous interaction phenomena in hypersonic wedge flow
    • Luigi de Luca, Gennaro Cardone, Dominique Chevalerie, and Alain Fonteneau. Viscous interaction phenomena in hypersonic wedge flow. AIAA Journal, 33(12) 2293-2299, December 1995.
    • (1995) AIAA Journal , vol.33 , Issue.12 , pp. 2293-2299
    • Luca, L.D.1    Cardone, G.2    Chevalerie, D.3    Fonteneau, A.4
  • 18
    • 0002286767 scopus 로고
    • On the Gortler instability of boundary layers
    • J. M. Floryan. On the Gortler instability of boundary layers. Progress in Aerospace Sciences, 28:235-271, 1991.
    • (1991) Progress in Aerospace Sciences , vol.28 , pp. 235-271
    • Floryan, J.M.1
  • 19
    • 0001314593 scopus 로고
    • A theoretical model of a wave packet in the boundary layer on a flat plate
    • M. Caster. A theoretical model of a wave packet in the boundary layer on a flat plate. Proc. Royal Soc. A, 347:271-289, 1975.
    • (1975) Proc. Royal Soc. A , vol.347 , pp. 271-289
    • Caster, M.1
  • 20
    • 0016484487 scopus 로고
    • Nozzle wall boundary-layer transition and freestream disturbances at Mach 5
    • W. D. Harvey, P. C. Stainback, J. B. Anders, and A. M. Gary. Nozzle wall boundary-layer transition and freestream disturbances at Mach 5. AIAA Journal, 13(3):307-314, 1975.
    • (1975) AIAA Journal , vol.13 , Issue.3 , pp. 307-314
    • Harvey, W.D.1    Stainback, P.C.2    Anders, J.B.3    Gary, A.M.4
  • 21
    • 0000746855 scopus 로고
    • Secondary instability of boundary layers
    • Th. Herbert. Secondary instability of boundary layers. Annual Reviews of Fluid Mechanics, 20:487-526, 1988.
    • (1988) Annual Reviews of Fluid Mechanics , vol.20 , pp. 487-526
    • Herbert, T.H.1
  • 23
    • 0004292957 scopus 로고
    • AGARD Report 793, Special Course on Progress in Transition Modelling
    • Th. Herbert. Parabolized stability equations. In AGARD Report 793, Special Course on Progress in Transition Modelling, pages 4/1-4/34., 1994.
    • (1994) Parabolized Stability Equations
    • Herbert, T.H.1
  • 25
    • 84983114194 scopus 로고
    • An exploratory study of transition on a slender cone in hypervelocity flow
    • R. Kobayashi, editor, Proceedings of the IUTAM Symposium held hi Sendai, Japan
    • H. G. Hornung and P. Germain. An exploratory study of transition on a slender cone in hypervelocity flow. In R. Kobayashi, editor, Laminar-Turbulent Transition, pages 155-162. Springer-Verlag, 1995. Proceedings of the IUTAM Symposium held hi Sendai, Japan, September 1994.
    • (1994) Laminar-Turbulent Transition , pp. 155-162
    • Hornung, H.G.1    Germain, P.2
  • 28
    • 12044253280 scopus 로고
    • Numerical simulation of transition in wall-bounded shear flows
    • L. Kleiser and T. Zang. Numerical simulation of transition in wall-bounded shear flows. Annual Reviews of Fluid Mechanics, 23:495-537, 1991.
    • (1991) Annual Reviews of Fluid Mechanics , vol.23 , pp. 495-537
    • Kleiser, L.1    Zang, T.2
  • 30
    • 0025508287 scopus 로고
    • Experiments on the stability of supersonic laminar boundary layers
    • A. Kosinov, A. Maslov, and S. Shevelkov. Experiments on the stability of supersonic laminar boundary layers. J. Fluid Mech., 219:621-633, 1990.
    • (1990) J. Fluid Mech. , vol.219 , pp. 621-633
    • Kosinov, A.1    Maslov, A.2    Shevelkov, S.3
  • 34
    • 84983181020 scopus 로고    scopus 로고
    • Technical report, Aerospace Sciences Laboratory, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana, 47907-1282, August 1994. 42 pages including 32 figures. Copies can be obtained from the authors
    • Dale W. Ladoon and S. P. Schneider. A high frequency glow discharge perturber for supersonic laminar-turbulent transition research. Technical report, Aerospace Sciences Laboratory, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana, 47907-1282, August 1994. 42 pages including 32 figures. Copies can be obtained from the authors.
    • A High Frequency Glow Discharge Perturber for Supersonic Laminar-Turbulent Transition Research
    • Ladoon, D.W.1    Schneider, S.P.2
  • 35
    • 84983125564 scopus 로고    scopus 로고
    • Aerospace Sciences Laboratory, School of Aeronautics and Astronautics, Purdue Univer-sity, west Lafayette, Indiana, 47907-1282 june 1995. 15 pages including 6 figures. Copies can be obtained from the authors
    • Dale W, Ladoon and S. P. Schneider. Preliminary tests of a glow discharge perturber in the Purdue quiet-flow Ludwieg tube. Technical report, Aerospace Sciences Laboratory, School of Aeronautics and Astronautics, Purdue Univer-sity, west Lafayette, Indiana, 47907-1282 june 1995. 15 pages including 6 figures. Copies can be obtained from the authors.
    • Preliminary Tests of a Glow Discharge Perturber in the Purdue Quiet-Flow Ludwieg Tube. Technical Report
    • Dale, W.1    Ladoonschneider, S.P.2
  • 36
    • 0001763901 scopus 로고
    • Aerodynamic noise in supersonic wind tunnels
    • John Laufer. Aerodynamic noise in supersonic wind tunnels. Journal of Aerospace Sciences, 28:685-692, 1961.
    • (1961) Journal of Aerospace Sciences , vol.28 , pp. 685-692
    • Laufer, J.1
  • 41
    • 84983186858 scopus 로고    scopus 로고
    • Proceedings of the Second Symposium on Transitional and Turbulent Compressible Flows, August 1995. A joint ASME/JSME Fluids Engineering Conference held at Hilton Head, S. C
    • Lan J. Lyttle and Helen L. Reed. Use of transition correlations for three-dimensional boundary layers within hypersonic viscous flows. In Proceedings of the Second Symposium on Transitional and Turbulent Compressible Flows, August 1995. A joint ASME/JSME Fluids Engineering Conference held at Hilton Head, S. C.
    • Use of Transition Correlations for Three-Dimensional Boundary Layers within Hypersonic Viscous Flows
    • Lyttle, L.J.1    Reed, H.L.2
  • 42
    • 0003631034 scopus 로고    scopus 로고
    • Special Course on Stability and Transition of Laminar Flow. Advisory Group for Aerospace Research and Development, 1984. AGARD Report No. 709
    • L. M. Mack. Boundary layer linear stability theory. In Special Course on Stability and Transition of Laminar Flow. Advisory Group for Aerospace Research and Development, 1984. AGARD Report No. 709.
    • Boundary Layer Linear Stability Theory
    • Mack, L.M.1
  • 43
    • 0024767419 scopus 로고
    • Malik. Prediction and control of transition in supersonic and hypersonic boundary layers
    • Mujeeb R. Malik. Prediction and control of transition in supersonic and hypersonic boundary layers. AIAA Journal, 27(11):1487-1493, November 1989.
    • (1989) AIAA Journal , vol.27 , Issue.11 , pp. 1487-1493
    • Mujeeb, R.1
  • 44
    • 36449001873 scopus 로고
    • Laminar flow control of subsonic boundary layers by suction and heat-transfer strips
    • J. A. Masad and A. H. Nayfeh. Laminar flow control of subsonic boundary layers by suction and heat-transfer strips. Physics of Fluids A, 4(6): 1259-1272, June 1992.
    • (1992) Physics of Fluids A , vol.4 , Issue.6 , pp. 1259-1272
    • Masad, J.A.1    Nayfeh, A.H.2
  • 45
    • 0001858503 scopus 로고
    • Bypass transition to turbulence and research desiderata
    • NASA CP-2386
    • Mark V. Morkovin. Bypass transition to turbulence and research desiderata. In Transition in Turbines, pages 161-199, 1985. NASA CP-2386.
    • (1985) Transition in Turbines , pp. 161-199
    • Morkovin, M.V.1
  • 46
    • 85014574593 scopus 로고
    • Note on the assessment of flow disturbances at a blunt body traveling at supersonic speeds owing to flow disturbances in free stream
    • M. V. Morkovin. Note on the assessment of flow disturbances at a blunt body traveling at supersonic speeds owing to flow disturbances in free stream. Journal of Applied Mechanics, pages 223-229, June 1960.
    • (1960) Journal of Applied Mechanics , pp. 223-229
    • Morkovin, M.V.1
  • 47
    • 0021938717 scopus 로고
    • The laminar-turbulent transition zone in the turbulent boundary layer
    • R. Narasimha. The laminar-turbulent transition zone in the turbulent boundary layer. Progress in Aerospace Science, 22:29-80, 1985.
    • (1985) Progress in Aerospace Science , vol.22 , pp. 29-80
    • Narasimha, R.1
  • 49
    • 85003342433 scopus 로고
    • Boundary-layer effects on pressure variations in Ludwieg tubes
    • E. Piltz. Boundary-layer effects on pressure variations in Ludwieg tubes. AIAA Journal, 10:1095-1097, 1972.
    • (1972) AIAA Journal , vol.10 , pp. 1095-1097
    • Piltz, E.1
  • 50
    • 84983138970 scopus 로고    scopus 로고
    • Master's thesis, Purdue University, School of Aeronautics and Astronautics, W. Lafayette, Indiana
    • Laura A. Randall. Receptivity of a hemispherical nose at Mach 4. Master's thesis, Purdue University, School of Aeronautics and Astronautics, W. Lafayette, Indiana, May 1996.
    • (1996) Receptivity of a Hemispherical Nose at Mach 4
    • Randall, L.A.1
  • 51
  • 52
    • 0003897928 scopus 로고
    • transition, and control. Paper 94-0001, AIAA, 1994, The, Dryden Lecture hi Research
    • Eli Reshotko. Boundary layer instability, transition, and control. Paper 94-0001, AIAA, 1994. The 1994 Dryden Lecture hi Research.
    • (1994) Boundary Layer Instability
    • Reshotko, E.1
  • 54
    • 0016597896 scopus 로고
    • Uniformity of Ludwieg tube flows
    • Proceedings of the 10th International Shock Tube Symposium, Kyoto
    • D. A. Russell, G. S. Knoke, and J. C. Wai. Uniformity of Ludwieg tube flows. In Modern Developments in Shock Tube Research, Proceedings of the 10th International Shock Tube Symposium, Kyoto, 1975.
    • (1975) Modern Developments in Shock Tube Research
    • Russell, D.A.1    Knoke, G.S.2    Wai, J.C.3
  • 57
    • 0029275740 scopus 로고
    • Improved methods for measuring laminar-turbulent intermittency in boundary layers
    • S. P. Schneider. Improved methods for measuring laminar-turbulent intermittency in boundary layers. Experiments in Fluids, 18:370-375, 1995.
    • (1995) Experiments in Fluids , vol.18 , pp. 370-375
    • Schneider, S.P.1
  • 58
    • 0029291727 scopus 로고
    • Quietflow Ludwieg tube for high-speed transition research
    • S.P. Schneider and C. E. Haven. Quietflow Ludwieg tube for high-speed transition research. AIAA Journal, 33(4):688-693, April 1995.
    • (1995) AIAA Journal , vol.33 , Issue.4 , pp. 688-693
    • Schneider, S.P.1    Haven, C.E.2
  • 66
    • 11444251496 scopus 로고    scopus 로고
    • USAF, NASA programs to push hypersonic boundaries
    • 6 May issue
    • W. Scott. USAF, NASA programs to push hypersonic boundaries. Aviation Week and Space Technology, 1996. 6 May issue, p. 22-23.
    • (1996) Aviation Week and Space Technology , pp. 22-23
    • Scott, W.1
  • 70
    • 84983143898 scopus 로고
    • Ames Research Staff. Equations, tables, and charts for compressible flow. Technical Report Report 1135
    • Ames Research Staff. Equations, tables, and charts for compressible flow. Technical Report Report 1135, National Advisory Committee for Aeronautics, 1952.
    • (1952) National Advisory Committee for Aeronautics
  • 71
    • 0026981575 scopus 로고
    • Example of second-mode instability dominance at a Mach number of 5. 2
    • K. F. Stetson and R. L. Kimmel. Example of second-mode instability dominance at a Mach number of 5. 2. AIAA Journal, 30(12):2974-2976, December 1992.
    • (1992) AIAA Journal , vol.30 , Issue.12 , pp. 2974-2976
    • Stetson, K.F.1    Kimmel, R.L.2
  • 73
    • 77956794244 scopus 로고
    • Condensation in supersonic and hypersonic wind tunnels
    • P. P. Wegener and L. M. Mack. Condensation in supersonic and hypersonic wind tunnels. Advances in Applied Mechanics, 5:307-447, 1958.
    • (1958) Advances in Applied Mechanics , vol.5 , pp. 307-447
    • Wegener, P.P.1    Mack, L.M.2
  • 76
    • 0029386276 scopus 로고
    • Nose cavity effects on blunt body pressure and temperatures at Mach 5
    • K. B. Yuceil and D. S. Dolling. Nose cavity effects on blunt body pressure and temperatures at Mach 5. J. Thermophysics and Heat Transfer, 9(4):612-619, 1995.
    • (1995) J. Thermophysics and Heat Transfer , vol.9 , Issue.4 , pp. 612-619
    • Yuceil, K.B.1    Dolling, D.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.