Transition due to heat-shield cavities on a Mars entry vehicle

Journal of Spacecraft and Rockets

Volumn 43, Issue 2, 2006, Pages 354-366

  Hollis, Brian R ^a,b,c   Liechty, Derek S ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Aerothermodynamics Branch   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; COMPUTATION THEORY; HEAT CONVECTION; NAVIER STOKES EQUATIONS; THERMOGRAPHY (TEMPERATURE MEASUREMENT); TURBULENCE; WIND TUNNELS;

BOUNDARY-LAYER TRANSITION; HEAT-SHIELD CAVITIES; LAMINAR HEATING DATA; NAVIER-STOKES COMPUTATIONS; PHOS-PHOR THERMOGRAPHY;

SPACECRAFT;

EID: 33646706820     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.19669     Document Type: Article

References (27)

1. Lockwood, M. K., Powell, R. W., Graves, C. A., and Carman, G. L., "Entry System Design Considerations for Mars Landers," American Astronautical Society, Paper AAS 01-023, Jan.-Feb. 2001.
2. Lockwood, M. K., Powell, R. W., Sutton, K., Prabhu, R. K., Graves, C. A., Epp, C. D., and Carman, G. L., "Entry Configurations and Performance Comparisons for the Mars Smart Lander," Journal of Spacecraft and Rockets, Vol. 43, No. 2, 2006, pp. 258-269.
3. Liechty, D. S., Hollis, B. R., and Edquist, K. T., "Mars Science Laboratory Experimental Aerothermodynamics with Effects of Cavities and Control Surfaces," Journal of Spacecraft and Rockets, Vol. 43, No. 2, 2006, pp. 340-353.
4. Edquist, K. T., Liechty, D. S., Hollis, B. R., Alter, S. J., and Loomis, M. P., "Aeroheating Environments for a Mars Smart Lander," Journal of Spacecraft and Rockets, Vol. 43, No. 2, 2006, pp. 330-339.
5. Cheatwood, F. M., Merski, N. M., Riley, C. J., and Mitchletree, R. A., "Aerothermodynamic Environment Definition for the Genesis Sample Return Capsule," AIAA Paper 2001-2889, June 2001.
6. Gnoffo, P. A., "An Upwind-Biased, Point-Implicit Algorithm for Viscous, Compressible Perfect-Gas Flows." NASA TP-2953, Feb. 1990.
7. Cheatwood, F. M., and Gnoffo, P. A., "User's Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA)," NASA TM 4674, April 1996.
8. Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors and Difference Schemes," Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372.
9. Harten, A., "High Resolution Schemes for Hyperbolic Conservation Laws," Journal of Computational Physics, Vol. 49, No. 3, 1983, pp. 357-393.
10. Yee, H. C., "On Symmetric and Upwind TVD Schemes," NASA TM 86842, Sept. 1985.
11. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow," AIAA Paper 78-257, Jan. 1978.
12. Cheatwood, F. M., and Thompson, R. A., "The Addition of Algebraic Turbulence Modeling to Program LAURA," NASA TM-107758, April 1993.
13. Dhawan, S., and Narashima, R., "Some Properties of Boundary Layer Flow from Laminar to Turbulent Motion," Journal of Fluid Mechanics, Vol. 1, Pt. 4, Jan. 1958, pp. 418-436.
14. Fay, J. A., and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," Journal of Aeronautical Sciences, Vol. 25, No. 2, 1958, pp. 73-85
15. Micol, J. R., "Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center: Aerothermodynamic Facilities Complex," AIAA Paper 95-2107, June 1995.
16. Micol, J. R., "Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities," AIAA Paper 98-0147, Jan. 1998.
17. Hollis, B. R., "Real-Gas Flow Properties for NASA Langley Research Center Aerothermodynamic Facilities Complex Wind Tunnels," NASA CR 4755. Sept. 1996.
18. Buck, G. M., "Automated Thermal Mapping Techniques Using Chromatic Image Analysis," NASA TM 101554, April 1989.
19. Buck, G. M., "Surface Temperature/Heat Transfer Measurement Using a Quantitative Phosphor Thermography System," AIAA Paper 91-0064, Jan. 1991.
20. Merski, N. R., "A Relative-Intensity, Two-Color Phosphor Thermography System," NASA TM 104123, Sept. 1991.
21. Merski, N. R., "Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Methods," Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 160-170.
22. Charwat, A. F., Roos, J. N., Dewey, C. F., and Hitz, J. A., "An Investigation of Separated Flows - Part I: The Pressure Field," Journal of the Aerospace Sciences, Vol. 28, No. 6, 1961, pp. 457-470.
23. Schiller, L., "Flow in Pipes," Handbook of Experimental Physics, Vol. 4, Pt. 4. Academic Press, Leipzig, Germany, 1932, pp. 189-192.
24. Reda, D. C., "Correlation of Nosetip Boundary-Layer Transition Data Measured in Ballistic Range Experiments," AIAA Journal, Vol. 19, No. 3, 1981, pp. 329-339.
25. Poll, D. I. A., "The Effect of Isolated Roughness Elements on Transition in Attachment-Line Flows," Laminar-Turbulent Transition, edited by D. Arnal and R. Michel, Springer-Verlag, New York, 1990, pp. 657-667.
26. Bouslog, S. A., Bertin, J. J., Berry, S. A., and Caram, J. M., "Isolated Roughness Induced Boundary-Layer Transition: Shuttle Orbiter Ground Tests and Experience," AIAA Paper 97-0274, Jan. 1997.
27. Berry, S. A., Bouslog, S. A., Brauckmann, G. J., and Caram, J. M., "Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness." Journal of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp. 241-248.