Blunt body near-wake flow field at mach 10

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages 1-27

  Horvath, Thomas ^a   Hannemannt, Klaus ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; FORECASTING; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; THERMOCOUPLES; WAKES;

AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; ANGLE OF INCIDENCE; LOCALIZED HEATING; NAVIER-STOKES CODE; PIEZORESISTIVE TRANSDUCERS; STAGNATION POINTS; SURFACE THERMOCOUPLES; TURBULENT SHEAR LAYER;

SHEAR FLOW;

EID: 84983208889     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (43)

1. Baker, P. J. and Martin, B. W. (1966): Heat Transfer in Supersonic Separated Flow Over A Two-Dimensional Backward-Facing Step. International Journal of Heat Mass Transfer, Vol. 9, p. 1081-1088.
2. Berger, Stanley A. (1971): Laminar Wakes. American Elsevier Publ., Inc.
3. 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.
4. 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, № 4/5.
5. Cook, William J. (1970): Unsteady Heat Transfer Measurements to a Semi-Infinite Solid With Arbitrary Surface Temperature History and Variable Thermal Properties. Iowa State Univ. Tech Report ISU-ERIAMES-67500.
6. Dye, T. P. (1993): An Experimental and Computational Investigation of the Flowfield About An Aeroassisted Space Transportation Vehicle at Mach 10. M. S. Thesis, University of Tennessee, Knoxville.
7. Faye-Petersen, R. (1972): Heat Transfer and Pressure Distributions at M-8 on 0.029 Scale Models of the Viking Entry Vehicle. NASA CR-132413, (Contract NAS1-9000).
8. Gochberg, L. A.; Alien, G. A.; Gallis, M. A.; and Deiwert, G. S. (1996): Comparison of Computations and Experiments For Nonequilibrium Flow Expansions Around A Blunted Cone. AIAA 34th Aerospace Sciences Meeting, Jan. 15-18, Reno, NV, AIAA 96-0231.
9. Gnoffo, P. A.; Price, J. M.; and Braun, R. D. (1992): Computation of Near-Wake, Aerobrake Flowfields. Journal of Spacecraft and Rockets, Vol. 29, №2.
10. Hama, Francis A. (1966): Experimental Investigations of Wedge Base Pressure and Lip Shock. Tech. Rep. № 32-1033 (Contract № NAS7-100), Jet Propulsion Lab., California Inst. of Technology.
11. Holden, M. S.; Chadwick, K. M.; Gallis, M. A., and Harvey, J. K. (1995): Comparison Between Shock Tunnel Measurements On A Planetary Probe Configuration and DSMC Predictions. Proceedings of the 20th Int. Sym. on Shock Waves, July 23-28, Pasadena, CA.
12. 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).
13. 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.
14. Hollis, Brian R. (1996): Experimental and Computational Aerothermodynamics of a Mars Entry Vehicle. Phd Dissertation, North Carolina State University. (Grant Nos. NAGl-1663, NAGW-1331).
15. Horvath, T. J.; McGinley, C. B.; and Hannemann, K. (1996): Blunt Body Near Wake Flow Field at Mach 6. 27th Fluid Dynamics Conference, June 18-20, New Orleans, LA, AIAA-1935.
16. Jones, Jim J. (1987): The Rationale for an Aeroassist Flight Experiment. AIAA 22th Thermophysics Conference, June 8-10, Honolulu, HI, AIAA-87-1508.
17. Kidd, C. T.; Nelson, C. G.; and Scott, W. T. (1995): Extraneous Thermoelectric EMF Effects Resulting From The Press-Fit Installation Of Coaxial Thermocouples in Metal Models. AEDC Rep. №, AAFB, TN.
18. Kastell, D.; Horvath T. J.; and Eitelberg G. (1994): Nonequilibrium Flow Expansion Around a Blunted Cone. 2nd European Symposium on Aerothermodynamics for Space Vehicles, Norwijk, NL.
19. Kastell, D.; Hannemann K.; Eitelberg G.; and Horvath T. J. (1995): Recompression of Nonequilibrium Flow in the Wake of a Blunted Cone. Proceedings of the 20th Int. Sym. on Shock Waves, July 23-28, Pasadena, CA.
20. Kendall, D. N.; Dixon, W. P.; and Schulte, E. H. (1967): Semiconductor Surface Thermocouples for Determining Heat-Transfer Rates. IEEE Transactions on Aerospace and Electronic Systems, Vol AES-3, № 4.
21. Kurotaki, T. (1996): Numerical Analysis of Thermochemical Nonequilibrium Hypersonic Flow Around Blunt Body. Proceedings of the 13th NAL Symposium on Aircraft Computational Aerodynamics, High Enthalpy Flow Workshop. SP-29, Tokyo.
22. 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.
23. Lees, L. (1964): Hypersonic Wakes and Trails. AIAA Journal, vol. 2, no. 3, pp.417-428.
24. Macaraeg, M. G. and Streett, C. L. (1991): Linear Stability of High-Speed Mixing Layers. Applied Numerical Mathematics, Vol. 7.
25. Mitcheltree, Robert A. (1994): Aerothermodynamic Methods for a Mars Environmental Survey Mars Entry. Journal of Spacecraft and Rockets, Vol. 31, № 3
26. Mitcheltree, Robert A. (1995): Computational Aerothermodynamics for Mars Pathfinder Including Turbulence. AIAA Atmospheric Flight Mechanics Conference, August 9, Baltimore, MD, AIAA-95-3493.
27. Miller, Charles G. III (1992): Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center. ALAA 17th Aerospace Ground Testing Conference, July 6-8, Nashville, TN, AIAA-92-3937.
28. Miller, Charles G. III (1981): Comparison of Thin-Film Resistance Heat-Transfer Gages With Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels. NASA TM 83197.
29. 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.
30. 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.
31. Reddy, N. M. and Miller, C. G. (1986): Study of Heating Distributions on a Family of Very Large Angle Cones. Unpublished NASA report.
32. Riedelbauch, S. and Brenner, G. (1990): Numerical Simulation of Laminar Hypersonic Flow Past Blunt Bodies Including High Temperature Effects. ALAA 21st Fluid Dynamics and Lasers Conference, Seattle, Washington, AIAA 90-1492.
33. Roe, P. L. (1981): Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes. J. Comp. Physics, Vol. 43, pp. 357-372.
34. Ronzheimer, A.; Brodersen, O.; Rudnik, R.; Findling, A.; and Rossow, C. (1994): A New Interactive Tool for the Management of Grid Generation Processes Around Arbitrary Configurations. 4th International Conference on Numerical Grid Generation in Computational Fluid Dynamics and Related Fields, Swansea UK, April 6-8.
35. Rosenhauer, M.; Wollenhaupt, M.; Scheer, M.; and Beck, W. H. (1994): LIF Measurements in the Wake of A Blunt Body In HEG. 2nd European Symposium on Aerothermodynamics for Space Vehicles, Norwijk, NL.
36. Saric, W. S. et al. (1996): Hypersonic Experimental and Computational Capability, Improvement and Validation. AGARD-AR-319 Vol 1.
37. Shimshi, J. P. (1992): An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack. M.S. Thesis, George Washington University.
38. Stewart, D. A. and Chen, Y. K. (1993): Convective Heat Transfer Rate Distributions Over a 140° Blunt Cone at Hypersonic Speeds in Different Gas Environments. AIAA 93-2787.
39. Tauber, M., et. al. (1993): MESUR Probe Aerobrake Preliminary Design Study. Journal of Spacecraft and Rockets, Vol. 30, №4.
40. Thornton, Aimee D. (1993): A Computational and Analytical Investigation of High Total-Enthalpy Supersonic Shear-Layer Data. MS Thesis, The George Washington University.
41. 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.
42. Wieting, Allan R. (1987): Experimental Study of Shock Wave Interference Heating on a Cylindrical Leading Edge. NASA TM 100484.
43. Yee, H. C. and Harten, A. (1987): Implicit TVD Schemes for Hyperbolic Conservation Laws in Curvilinear Coordinates. AIAA Journal Vol. 25, pp. 266-274.