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Volumn , Issue , 1996, Pages 1-33

Blunt body near-wake flow field at mach 6

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; HEATING; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHOCK TESTING; SURVEYS; THERMOCOUPLES; WAKES; WELL TESTING;

EID: 33751398901     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1935     Document Type: Conference Paper
Times cited : (9)

References (41)
  • 1
    • 0024139525 scopus 로고
    • Miniaturized Compact Water-Cooled Pitot-Pressure Probe for Flow-Field Surveys in Hypersonic Wind Tunnels
    • Ashby, George C Jr. (1988): Miniaturized Compact Water-Cooled Pitot-Pressure Probe for Flow-Field Surveys in Hypersonic Wind Tunnels. ISA 34th Int. Instr. Sym.
    • (1988) ISA 34Th Int. Instr. Sym
    • Ashby, G.C.1
  • 2
    • 6244230371 scopus 로고
    • Heat Transfer in Supersonic Separated Flow Over A Two-Dimensional Backward-Facing Step
    • Baker, P. J., and Martin, B.W. (1966): Heat Transfer in Supersonic Separated Flow Over A Two-Dimensional Backward-Facing Step. Int.J. Heat Mass Transfer, Vol. 9, p. 1081-1088.
    • (1966) Int.J. Heat Mass Transfer , vol.9 , pp. 1081-1088
    • Baker, P.J.1    Martin, B.W.2
  • 3
    • 0003955643 scopus 로고
    • American Elsevier Publ., Inc
    • Berger, Stanley A. (1971): Laminar Wakes. American Elsevier Publ., Inc.
    • (1971) Laminar Wakes
    • Berger, S.A.1
  • 4
    • 85006150709 scopus 로고
    • Numerical Simulation of Chemical and Thermal Nonequilibrium Flows after Compression Shocks
    • July 6-8, Nashville, TN, AIAA
    • Brenner, G. and Prinz, U. (1992): Numerical Simulation of Chemical and Thermal Nonequilibrium Flows after Compression Shocks. AIAA 27th Thermophysics Conference, July 6-8, Nashville, TN, AIAA 92-2879.
    • (1992) AIAA 27Th Thermophysics Conference , pp. 92-2879
    • Brenner, G.1    Prinz, U.2
  • 5
    • 0027625342 scopus 로고
    • Numerical Simulation of Shock/Shock and Shock-Wave/Boundary-Layer Interactions in Hypersonic Flows
    • Brenner, G., Gerhold, T., Hannemann, K., and Rues, D. (1993): Numerical Simulation of Shock/Shock and Shock-Wave/Boundary-Layer Interactions in Hypersonic Flows. Computers & Fluids, Vol. 22, No. 4/5.
    • (1993) Computers & Fluids , vol.22 , Issue.4-5
    • Brenner, G.1    Gerhold, T.2    Hannemann, K.3    Rues, D.4
  • 10
    • 84968542373 scopus 로고
    • Mars Pathfinder Computations Including Base-Heating Predictions
    • June 19-22, San Diego, CA., AIAA 95-2086
    • Haas, B. L. and Venkatapathy, E. (1995): Mars Pathfinder Computations Including Base-Heating Predictions. AIAA 30th Thermophysics Conference, June 19-22, San Diego, CA., AIAA 95-2086.
    • (1995) AIAA 30Th Thermophysics Conference
    • Haas, B.L.1    Venkatapathy, E.2
  • 11
    • 6244253446 scopus 로고
    • Tech. Rep. No. 32-1033 (Contract No. NAS7-100), Jet Propulsion Lab., California Inst. of Technology
    • Kama, Francis A. (1966): Experimental Investigations of Wedge Base Pressure and Lip Shock. Tech. Rep. No. 32-1033 (Contract No. NAS7-100), Jet Propulsion Lab., California Inst. of Technology.
    • (1966) Experimental Investigations of Wedge Base Pressure and Lip Shock
    • Kama, F.A.1
  • 12
    • 84964288261 scopus 로고
    • The Turbulence Structure of A Reattaching Axisymmetric Supersonic Free Shear Layer
    • June 19-22, San Diego, CA., AIAA-95-2250
    • Herrin, J.L. and Dutton, J.C. (1995): The Turbulence Structure of A Reattaching Axisymmetric Supersonic Free Shear Layer. AIAA 26th Fluid Dynamics Conference, June 19-22, San Diego, CA., AIAA-95-2250.
    • (1995) AIAA 26Th Fluid Dynamics Conference
    • Herrin, J.L.1    Dutton, J.C.2
  • 13
    • 0343834707 scopus 로고
    • Penetration Performance of Segmented Rods at Different Spacing- Comparison with Homogeneous Rods at 2.5-3.5 km/s
    • Hohler, V. and Stilp, A. (1990): Penetration Performance of Segmented Rods at Different Spacing- Comparison with Homogeneous Rods at 2.5-3.5 km/s. Proceedings of the 12th Int. Sym. On Ballistics, Vol. 78, No. 12.
    • (1990) Proceedings of the 12Th Int. Sym. on Ballistics , vol.78 , Issue.12
    • Hohler, V.1    Stilp, A.2
  • 14
  • 15
    • 0345160052 scopus 로고
    • User's Manual for the One-Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) Data Reduction Code
    • (Grant Nos. NAGl-1663, NAGW-1331)
    • Hollis, Brian R. (1995): User's Manual for the One-Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) Data Reduction Code. NASA CR 4691, (Grant Nos. NAGl-1663, NAGW-1331).
    • (1995) NASA CR , vol.4691
    • Hollis, B.R.1
  • 16
    • 84959250155 scopus 로고
    • Hypervelocity Aeroheating Measurements in Wake of Mars Mission Entry Vehicle
    • June 19-22, San Diego, CA., AIAA-95-2314
    • Hollis, B.R. and Perkins, J.N.(1995): Hypervelocity Aeroheating Measurements in Wake of Mars Mission Entry Vehicle. AIAA 26th Fluid Dynamics Conference, June 19-22, San Diego, CA., AIAA-95-2314.
    • (1995) AIAA 26Th Fluid Dynamics Conference
    • Hollis, B.R.1    Perkins, J.N.2
  • 17
    • 84997831514 scopus 로고
    • The Rationale for an Aeroassist Flight Experiment
    • June 8-10, Honolulu, HI., AIAA-87-1508
    • Jones, Jim J. (1987): The Rationale for an Aeroassist Flight Experiment. AIAA 22th Thermophysics Conference, June 8-10, Honolulu, HI., AIAA-87-1508.
    • (1987) AIAA 22Th Thermophysics Conference
    • Jones, J.J.1
  • 21
    • 0027964097 scopus 로고
    • Extraneous Thermoelectric EMF Effects Resulting From The Press-Fit Installation Of Coaxial Thermocouples in Metal Models
    • Baltimore, MD
    • Kidd, C.T., Nelson, C.G., and Scott, W.T. (1994).: Extraneous Thermoelectric EMF Effects Resulting From The Press-Fit Installation Of Coaxial Thermocouples in Metal Models. Proceedings of the 40th International Instrumentation Symposium, Baltimore, MD.
    • (1994) Proceedings of the 40Th International Instrumentation Symposium
    • Kidd, C.T.1    Nelson, C.G.2    Scott, W.T.3
  • 22
    • 84963614659 scopus 로고
    • Numerical Investigation of Laminar-Turbulent Transition in the Boundary-Layer of Reentry Capsules
    • January 9-12, Reno, NV., AIAA-95-0775
    • Laurien E. (1995): Numerical Investigation of Laminar-Turbulent Transition in the Boundary-Layer of Reentry Capsules. AIAA 33rd Aerospace Sciences Meeting, January 9-12, Reno, NV., AIAA-95-0775.
    • (1995) AIAA 33Rd Aerospace Sciences Meeting
    • Laurien, E.1
  • 24
    • 0028423737 scopus 로고
    • Aerothermodynamic Methods for a Mars Environmental Survey Mars Entry
    • Mitcheltree, Robert A. (1994): Aerothermodynamic Methods for a Mars Environmental Survey Mars Entry. J. of Spacecraft and Rockets, Vol. 31, No. 3.
    • (1994) J. of Spacecraft and Rockets , vol.31 , Issue.3
    • Mitcheltree, R.A.1
  • 25
    • 0344840867 scopus 로고
    • Computational Aerothermodynamics for Mars Pathfinder Including Turbulence
    • August 9, Baltimore, MD, AIAA-95-3493
    • Mitcheltree, Robert A. (1995): Computational Aerothermodynamics for Mars Pathfinder Including Turbulence. AIAA Atmospheric Flight Mechanics Conference, August 9, Baltimore, MD, AIAA-95-3493.
    • (1995) AIAA Atmospheric Flight Mechanics Conference
    • Mitcheltree, R.A.1
  • 26
    • 29644446911 scopus 로고
    • Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center
    • July 6-8, Nashville, TN., AIAA-92-3937
    • Miller, Charles G. Ill (1992): Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center. AIAA 17th Aerospace Ground Testing Conference, July 6-8, Nashville, TN., AIAA-92-3937.
    • (1992) AIAA 17Th Aerospace Ground Testing Conference
    • Miller, C.G.I.1
  • 27
    • 0342601842 scopus 로고
    • Comparison of Thin-Film Resistance Heat-Transfer Gages With Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels
    • Miller, Charles G. Ill (1981): Comparison of Thin-Film Resistance Heat-Transfer Gages With Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels. NASA TM 83197.
    • (1981) NASA TM , pp. 83197
    • Miller, C.G.I.1
  • 28
    • 85002263338 scopus 로고
    • Hypersonic Blunt Body Wake Computations Using DSMC and Navier-Stokes Solvers
    • July 6-9, Orlando, FL. AIAA-93-2807
    • Moss, J.N., Mitcheltree, R.A., and Wilmoth, R.G. (1993): Hypersonic Blunt Body Wake Computations Using DSMC and Navier-Stokes Solvers. AIAA 28th Thermophysics Conference, July 6-9, Orlando, FL. AIAA-93-2807.
    • (1993) AIAA 28Th Thermophysics Conference
    • Moss, J.N.1    Mitcheltree, R.A.2    Wilmoth, R.G.3
  • 29
    • 84959240298 scopus 로고
    • DSMC Calculations for a 70° Blunted Cone at 3.2 km/s in Nitrogen
    • Moss, J.N., Price, J.M., and Dogra, V.K. (1995): DSMC Calculations for a 70° Blunted Cone at 3.2 km/s in Nitrogen. NASA TM 109181.
    • (1995) NASA TM
    • Moss, J.N.1    Price, J.M.2    Dogra, V.K.3
  • 30
    • 84959240340 scopus 로고
    • Measurements of Heat Transfer in Bubbles of Separated Flow in Supersonic Air Streams
    • London
    • Naysmith, A. (1961): Measurements of Heat Transfer in Bubbles of Separated Flow in Supersonic Air Streams. ASME & Instn. Mech. Engrs., Int. Heat Transfer Conf., Part II, London.
    • (1961) ASME & Instn. Mech. Engrs., Int. Heat Transfer Conf
    • Naysmith, A.1
  • 31
    • 85006410971 scopus 로고
    • Numerical Simulation of Laminar Hypersonic Flow Past Blunt Bodies Including High Temperature Effects
    • Seattle, Washington, AIAA
    • Riedelbauch, S and Brenner, G. (1990): Numerical Simulation of Laminar Hypersonic Flow Past Blunt Bodies Including High Temperature Effects. AIAA 21st Fluid Dynamics and Lasers Conference, Seattle, Washington, AIAA 90-1492.
    • (1990) AIAA 21St Fluid Dynamics and Lasers Conference , pp. 90-1492
    • Riedelbauch, S.1    Brenner, G.2
  • 32
    • 2942757053 scopus 로고
    • Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes
    • Roe, P. L. (1981): Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes. J. Comp. Physics, Vol. 43, pp. 357-372.
    • (1981) J. Comp. Physics , vol.43 , pp. 357-372
    • Roe, P.L.1
  • 36
    • 84959223298 scopus 로고
    • The measurement of disturbance levels in the langley research center 20-inch mach 6 tunnel
    • Stainback, P.O. and Kubendran, L.R. (1994) The Measurement of Disturbance Levels in the Langley Research Center 20-Inch Mach 6 Tunnel. NASA CR 4571, NAS1- 19320.
    • (1994) NASA CR 4571, NAS1- 19320
    • Stainback, P.O.1    Kubendran, L.R.2
  • 37
    • 84959239789 scopus 로고
    • Mesur probe aerobrake preliminary design study
    • Tauber, M., et al (1993): MESUR Probe Aerobrake Preliminary Design Study. J. Spacecraft and Rockets,Vol. 30, No.4.
    • (1993) J. Spacecraft and Rockets , vol.30 , Issue.4
    • Tauber, M.1
  • 39
    • 84959232330 scopus 로고
    • Surface flow and heating distributions on a cylinder in near wake of aeroassist flight experiment (Afe) configuration at incidence in mach 10 air
    • Wells, William L. (1990): Surface Flow and Heating Distributions on a Cylinder in Near Wake of Aeroassist Flight Experiment (AFE) Configuration at Incidence in Mach 10 Air. NASA TP 2954.
    • (1990) NASA TP , pp. 2954
    • Wells, W.L.1
  • 40
    • 79955877519 scopus 로고
    • Experimental study of shock wave interference heating on a cylindrical leading edge
    • Wieting, Allan R. (1987): Experimental Study of Shock Wave Interference Heating on a Cylindrical leading Edge. NASA TM 100-484.
    • (1987) NASA TM , pp. 100-484
    • Wieting, A.R.1
  • 41
    • 0023295524 scopus 로고
    • Implicit tvd schemes for hyperbolic conservation laws in curvilinear coordinates
    • Yee, H. C. and Harten, A. (1987): Implicit TVD Schemes for Hyperbolic Conservation Laws in Curvilinear Coordinates. AIAA J., Vol. 25, pp. 266-274.
    • (1987) AIAA J , vol.25 , pp. 266-274
    • Yee, H.C.1    Harten, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.