Plume-on base drag prediction including three-dimensional and real-gas effects

Journal of Spacecraft and Rockets

Volumn 38, Issue 2, 2001, Pages 136-142

  Rubio, G ^a,b   Matesanz, A ^b   Velazquez A ^a,b  

^a UNIVERSIDAD CARLOS III DE MADRID   (Spain)

^b SENER Ingenieria y Sistemas SA   (Spain)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; DRAG; ITERATIVE METHODS; NOZZLES; PRESSURE EFFECTS; THERMAL PLUMES;

AERODYNAMIC INTERACTIONS;

SPACE FLIGHT;

EID: 0035269741     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3680     Document Type: Article

References (36)

1. Tang, H. H., and Barnes, J. W., "A Combining Parameter for Base Pressure Evaluation," AIAA Journal, Vol. 5, No. 9, 1967, pp. 1722-1724.
2. Addy, A. L., "Experimental-Theoretical Correlation for Supersonic Jet-On Base Pressure for Cylindrical Afterbodies," Journal of Aircraft, Vol. 7, No. 5, 1970, pp. 474-477.
3. Su, M. W., and Wu, J. M., "Base Pressure Correlation in Supersonic Flow," AIAA Journal, Vol. 9, No. 7, 1971, pp. 1429-1431.
4. Kawecki, E. J., "Comparison of Several Re-Entry Vehicle Base Pressure Correlations," Journal of Spacecraft, Vol. 14, No. 5, 1977, pp. 284-289.
5. Brazzel, C. E., and Henderson, J. H., "An Empirical Technique for Estimating Power-on Base Drag of Bodies of Revolution with a Single Jet Exhaust," CP-10, AGARD, 1966.
6. Tanner M., "Theoretical Prediction of Base Pressure for Steady Base Flows," Progress in Aerospace Sciences, Vol. 14, 1973, pp. 177-225.
7. Lamb, J. P., and Oberkampf, W. L., "Review and Development of Base Pressure and Base Heating Correlations in Supersonic Flow," Journal of Spacecraft and Rockets, Vol. 32, No. 1, 1995, pp. 8-23.
8. Chapman, A. J., and Korst, H. H., "Free Jet Boundary with Consideration of Initial Boundary Layer," Second U.S. National Congress of Applied Mechanics, June 1954.
9. Korst, H. H., Chow W. L., and Zumwalt G. W., "Research on Transonic and Supersonic Flow of a Real Fluid at Abrupt Increases in Cross-Section - Final Report," Mechanical Engineering Technical Rept. 392-5, Univ. of Illinois, Urbana, IL, Dec. 1959.
10. Korst, H. H., "A Theory for Base Pressures in Transonic and Supersonic Flow," Journal of Applied Mechanics, Vol. 23, No. 4, 1956, pp. 593-600.
11. Alber, I. E., and Lees, L., "Integral Theory for Supersonic Turbulent Base Flows," AIAA Journal, Vol. 6, No. 7, 1968, pp. 1343-1351.
12. Fox, J. H., "Simple Recompression Model for the Korst Base Pressure Theory," AIAA Journal, Vol. 17, No. 3, 1979, pp. 311-313.
13. Addy, A. L., Dutton, J. C., and Amatucci, V. A., "Nonuniform Nozzle Flow Effects on Base Pressure at Supersonic Flight Speeds," AIAA Journal, Vol. 24, No. 7, 1986, pp. 1209-1212.
14. Schetz, J. A., Billig, F. S., and Favin, S., "Simplified Analysis of Supersonic Base Flows Including Injection and Combustion," AIAA Journal Vol. 14, No. 1, 1978, pp. 7, 8.
15. Weng, C. H., and Chow, W. L., "Axisymmetric Supersonic Turbulent Base Pressure," AIAA Journal, Vol. 16, No. 6, 1978, pp. 553, 554.
16. Tanner, M., "Boundary Layer Thickness and Base Pressure," AIAA Journal, Vol. 23, No. 12, 1985, pp. 1987-1989.
17. Wagner, B., and White, R. A., "Supersonic Base Flow Problem in Presence of an Exhaust Jet," AIAA Journal, Vol. 18, No. 8, 1980, pp. 876-882.
18. Hwang, C. B., Chow, W. L., and Moslemian, D., "Base Pressure of a Sudden Expansion from a Conical Converging Nozzle," AIAA Journal, Vol. 31, No. 4, 1993, pp. 657-662.
19. Reijasse, P. R., Benay, R., Delery, J. M., and Lacau, R. G., "Missile and Projectile Base-Flow Prediction by Multicomponent Methods," AIAA Paper 88-4380, Aug. 1988.
20. Delery J., and Wagner, B., "Results of Garteur Action Group AG09 on Flow Past Missile Afterbodies," Missile Aerodynamics, CP-493, AGARD, 1990, pp. 25-1, 25-35.
21. Jenn, A., "Drag Prediction Methods for Axisymmetric Missile Bodies," Tactical Missile Aerodynamics: Prediction Methodology, Vol. 142, edited by M. R. Mendenhall, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1991, pp. 37-62.
22. Sahu, J., "Numerical Computations of Supersonic Base Flow with Special Emphasis on Turbulence Modelling," AIAA Journal, Vol. 32, No. 7, 1994, pp. 1547-1549.
23. Chuang, C. C., and Chieng, C. C., "Supersonic Base-Flow Computation Using Higher-Order Closure Turbulence Models," Journal of Spacecraft and Rockets, Vol. 33, No. 3, 1996, pp. 374-380.
24. Wang, T.-S., "Grid-Resolved Analysis of Base Flowfield for Four-Engine Clustered Nozzle Configuration," Journal of Spacecraft and Rockets, Vol. 33, No. 1, 1996, pp. 22-29.
25. Sahu, J., and Heavey, K. R., "Numerical Investigation of Supersonic Base Flow with Base Bleed," Journal of Spacecraft and Rockets, Vol. 34, No. 1, 1997, pp. 62-69.
26. Dash, S. M., and Sinha, N., "Exhaust Plumes and Their Interaction with Missile Airframes: A New Viewpoint," Tactical Missile Aerodynamics: Prediction Methodology, Vol. 142, edited by M. R. Mendenhall, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1991, pp. 649-756.
27. Sillen, M., "Investigation of Base Flow on a Space Rocket with Plumes," AIAA Paper 98-1599, April 1998.
28. Matesanz, A., Velázquez, A., "EARSM Finite Element Solver for the Study of Turbulent 3-D Compressible Separated Flows," Computer Methods in Applied Mechanics and Engineering, Vol. 190, No. 8-10, 2000, pp. 989-1004.
29. Délery, J., and Lacau, R.-G., "Prediction of Base Flows," Special Course on Missile Aerodynamics, AGARD Rept. 754, 1988.
30. Mueller, J. S., Hall, C. R., Jr., and Roache, P. J., "The Influence of Initial Flow Direction on the Turbulent Base Pressure in Supersonic Axisymmetric Flow" Journal of Spacecraft, Vol. 7, No. 12, 1970, pp. 1484-1488.
31. Englert, C. W., Vargo, D. J., and Cubbison, R. W., "Effect of Jet-Nozzle-Expansion Ratio on Drag of Parabolic Afterbodies," NACA RM E54B12, April 1959.
32. Bannink, W. J., Houtmann, E. M., and Bakker, P. G., "Base Flow/Underexpanded Exhaust Plume Interaction in a Supersonic External Flow," AIAA Paper 98-1598, April 1998.
33. Matesanz, A., Velázquez, A., Jiménez, A., and Rodríguez, M., "Numerically Robust 3-D Finite Element Reynolds Averaged Navier Stokes Solver for the Study of Turbulent Supersonic External Flows," Computer Method in Applied Mechanics and Engineering, No. 3-4, July 1998, pp. 383-394.
34. Herrin, J. L., and Dutton, J. C., "Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody," AIAA Journal, Vol. 32, No. 1, 1994, pp. 77-83.
35. Herrin, J. L., and Dutton, J. C., "Supersonic Near-Wake Afterbody Boattailing Effects on Axisymmetric Bodies," Journal of Spacecraft and Rockets, Vol. 31, No. 6, 1994, pp. 1021-1027.
36. Moore, F. G., Hymer, T., and Wilcox, F. J., "Improved Empirical Model for Base Drag Prediction on Missile Configurations Based on New Wind Tunnel Data," U.S. Naval Surface Warfare Center, Rept. NSWCDD/TR-92/509, Washington, DC, Oct. 1992.