Estimation methods for two-dimensional conduction effects of shock-shock heat fluxes

Journal of thermophysics and heat transfer

Volumn 14, Issue 4, 2000, Pages 533-539

  Walker, D Greg ^a   Scott, Elaine P ^b   Nowak, Robert J ^c  

^a VANDERBILT UNIVERSITY   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; HEAT FLUX; HYPERSONIC FLOW; INVERSE PROBLEMS;

SHOCK-SHOCK HEAT FLUXES; TWO-DIMENSIONAL CONDUCTION EFFECTS;

HEAT CONDUCTION;

EID: 0034297669     PISSN: 08878722     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.6554     Document Type: Article

References (22)

1. Burcham, F. W., Jr., and Nugent, J., "Local Flowfield Around a PylonMounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7," NASA TN D-5638, 1970.
2. Watts, J. D., "Flight Experience with Shock Impingement and Interface Heating on the X-15-2 Research Airplane," NASA TM X-1669, Oct. 1968.
3. Prabhu, R. K., "An Implementation of a Chemical and Thermal Nonequilibrium Flow Solver on Unstructured Meshes and Application to Blunt Bodies," NASA CR 194967, Aug. 1994.
4. Hiers, R. S., and Loubsky, W. J., Effects of Shock-Wave Impingement on the Heat Transfer on a Cylindrical Leading Edge," NASA TN D-3859, 1967.
5. Edney, B. E., "Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock," Aeronautical Research Inst. of Sweden, Bromma, Sweden, FFA Rept. 115, Feb. 1968.
6. Wieting, A. R., and Holden, M.S., "Experimental Study of Shock Wave Interference Heating on a Cylindrical Leading Edge at Mach 6 and 8,© AIAA Journal, Vol. 27, No. 11, 1989, pp. 1557-1565.
7. Kolly, J., Nowak, R., and Holden, M., "Experiments on the Effects of Reynolds Number and Turbulence in Hypersonic Shock-Shock Interactions," AIAA Paper 97-1882, June-July 1997.
8. Berry, S. A., and Nowak, R. J., "Effects of Fin Leading-Edge Sweep on Shock-Shock Interaction at Mach 6," Journal of Spacecraft and Rockets, Vol. 34, No. 4, 1997, pp. 416-425.
9. Neumann, R. D., "High-Speed Shock Impingement Studies Using Innovative Movement of Model Components to Expedite Testing in Traditional Wind-Tunnel Facilities," AIAA Paper 96-2192, June 1996.
10. Glass, C. E., Wieting, A. R., and Holden, M. S., "Effect of Leading-Edge Sweep on Shock-Shock Interference at Mach 8," AIAA Paper 89-0271, Jan. 1989.
11. Wright, M. J., Nowak, R. J., Berry, S. A., Glass, C. E., and Candler, G. V., "Numerical/Experimental Investigation of Three-Dimensional Swept Fin Shock Interactions," AIAA Paper 98-2816, June 1998.
12. Ehrich, F. F., "Differentiation of Experimental Data Using Least Squares Fitting," Journal of the Aeronautical Sciences, Vol. 22, No. 2, 1954, pp. 133, 134.
13. Beck, J. V., Blackwell, B., and St. Clair, C. R., Jr., Inverse Heat Conduction: III-Posed Problems, Wiley, New York, 1985, pp. 2, 3.
14. Walker, D. G., and Scott, E. P., "Evaluation of Estimation Methods for High Unsteady Heat Fluxes from Surface Measurements," Journal of Thermophysics and Heat Transfer, Vol. 12, No. 4, 1998, pp. 543-551.
15. Walker, D. G., and Scott, E. P., "One-Dimensional Heat Flux History Estimation from Discrete Temperature Measurements," American Society of Mechanical Engineers, Paper 317-1, p. 175, Nov. 1995.
16. Diller, T. E., "Methods of Determining Heat Flux from Temperature Measurements," 43rd International Instrumentation Symposium, Instrument Society of America, Orlando, FL, 1996, pp. 357-369.
17. Walker, D. G., and Scott, E. P., "A Method for Improving Two-Dimensional High Heat Flux Estimates from Surface Temperature Measurements," AIAA Paper 97-2574, June 1997.
18. Hollis, B. R., "User's Manual for the One-Dimensional Hypersonic Experimental Aerothermodynamic (1DHEAT) Data Reduction Code," NASA CR 4691, 1995.
19. Diller, T. E., and Kidd, C. T., "Evaluation of Numerical Methods for Determining Heat Flux with a Null Point Calorimeter," 42nd International Instrumentation Symposium, Instrument Society of America, Research Triangle Park, NC 1997, pp. 251-262.
20. Scott, E. P., and Beck, J. V., "Analysis of Order of the Sequential Regularization Solutions of Inverse Heat Conduction Problems," Journal of Heat Transfer, Vol. 111, No. 2, 1987, pp. 218-224.
21. Buttsworth, D. R., and Jones, T. V., "Radial Conduction Effects in Transient Heat Transfer Experiments," Aeronautical Journal, Vol. 101, No. 1005, 1997, pp. 209-212.
22. Haftka, R. T., Scott, E. P., and Cruz, J. R., "Optimizations and Experiments: A Survey," Applied Mechanics Reviews, Vol. 51, No. 7, 1998, pp. 435-448.