Skin-friction prediction for high-speed turbulent boundary layers with ablation

Journal of Spacecraft and Rockets

Volumn 41, Issue 5, 2004, Pages 893-895

  Fang, Yichuan ^a,c   Liou, William W ^a,c   Xu, Shuxuan ^b,c  

^a WESTERN MICHIGAN UNIVERSITY   (United States)

^b UNIVERSITY OF SCIENCE AND TECHNOLOGY OF CHINA   (China)

^c Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; HEAT TRANSFER; MISSILE LAUNCHING SYSTEMS; PRESSURE EFFECTS; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; SURFACE ROUGHNESS; TEMPERATURE CONTROL;

AEROTHERMODYNAMICS; SKIN FRICTION; SURFACE EROSION; TURBULENT BOUNDARY LAYERS;

FRICTION;

EID: 7544240472     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.8593     Document Type: Article

References (23)

1. Nikuradse, J., "Stromungsgesetze in Rauhen Rohren," VDI Forshungsheft, Series B, Vol. 4, No. 361, 1933; English translation, NACA TM1292, 1950.
2. Nikuradse, J., "Stromungsgesetze in Rauhen Rohren," VDI Forshungsheft, Series B, Vol. 4, No. 361, 1933; English translation, NACA TM1292, 1950.
3. Schlichting, H., Boundary Layer Theory, 4th ed., McGraw-Hill, New York, 1960, p. 616.
4. Holden, M. S., "Experimental Studies of Surface Roughness Shape and Spacing Effects on Heat Transfer and Skin Friction in Supersonic and Hypersonic Flows," AIAA Paper 84-0016, 1984.
5. Keel, A. G., "Influence of Surface Roughness on Skin Friction and Heat Transfer for Compressible Turbulent Boundary Layers," AIAA Paper 77-0178, 1977.
6. Holden, M. S., Neumann, R. D., Burke, J., and Rodriguez, K. M., "An Experimental Study of the Effect of Injectant Properties on the Aerothermal Characteristics of Transpiration Cooled Cones in Hypersonic Flow," AIAA Paper 90-1487, 1990.
7. Timmer, H. G., Arne, C. L., Stokes, T. R., and Tang, H. H., "Aerothermodynamic Characteristics of Slender Ablating Re-Entry Vehicles," AIAA Paper 70-826, 1970.
8. Laganelli, A. L., Fogaroli, R. P., and Martellucci, A., "The Effect of Mach Number and Wall Temperature on Turbulent Heat Blockage Resulting from Mass Injection," AIAA Paper. 78-784, 1978.
9. Lees, L., and Chapkis, R. L., "Surface Mass Injection at Supersonic and Hypersonic Speed as a Problem in Turbulent Mixing, Part II: Axially-Symmetric Flow," AIAA Journal, Vol. 9, No. 6, 1971, pp. 1067-1074.
10. Lin, T. C., Sproul, L., and Olmos, M., "An Aerothermal Model For Ablation Heat Shields," AIAA Paper 94-0247, 1994.
11. Jeromin, L. O. F., "The Status of Research in Turbulent Boundary Layers with Fluid Injection," Progress in Aeronautical Sciences, Vol. 10, 1970, pp. 76-189.
12. Kuntz, D. W., Hassan, B., and Potter, D. L., "Predictions of Ablating Hypersonic Vehicles Using an Iterative Coupling Fluid/Thermal Approach," Journal of Thermophysics and Heat Transfer, Vol. 15, No. 2, 2001, pp. 129-139.
13. Chen, Y.-K., and Milos, F. S., "Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials," Journal of Spacecraft and Rockets, Vol. 38, No. 4, 2001, pp. 473-481.
14. Chen, Y.-K., and Milos, F. S.,'"Ablation and Thermal Response Program for Spacecraft Heatshield Analysis," Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 475-483.
15. Izawa, Y., and Sawada, K., "Calculation of Hypersonic Flow with Ablation for Pioneer-Venus Probe," AIAA Paper 2000-0208, 2000.
16. Voisinet, R. L. P., "Combined Influence of Roughness and Mass Transfer on Turbulent Skin Friction at Mach 2.9," U.S. Naval Surface Weapons Center, NSWC TR-79-153, White Oak, MD, June 1979.
17. Holden, M. S., "Studies of Surface Roughness and Blowing Effects on Hypersonic Turbulent Boundary Layers over Slender Cones," AIAA Paper 89-0458, 1989.
18. Laganelli, A. L., and Sontowski, J., "Prediction of Skin Friction with Coupled Roughness and Blowing Based on Transformation Functions," AIAA Paper 82-0033, 1982.
19. Goddard, F. E., Jr., "Effect of Uniformly Distributed Roughness on Turbulent Skin-Friction Drag at Supersonic Speed," Journal of Aerospace Sciences, Vol. 26, No.1, 1959, pp. 1-15.
20. Nestler, D. E., "Compressible Turbulent Boundary Layer Heat Transfer to Rough Surface," AIAA Journal, Vol. 9, No. 9, 1971, pp. 1799-1803.
21. Kutateladze, S. S., and Leontiev, A. I., Turbulent Boundary Layers in Compressible Gases, Academic Press, New York, 1964.
22. Marvin, J. G., and Pope, R. B., "Laminar Convective Heating and Ablation in the Mars Atmosphere," AIAA Journal, Vol. 5, No. 2, 1967, pp. 240-248.
23. Gross, J. F., "A Review of Binary Laminar Boundary Layer Characteristics," International Journal of Heat and Mass Transfer, Vol. 3, No. 3, 1961, pp. 210-215.