Rapid engineering approach to modeling hypersonic laminar-to-hirbulent transitional flows

Journal of Spacecraft and Rockets

Volumn 42, Issue 3, 2005, Pages 467-475

  Papp, J L ^a,b   Dash, S M ^a,b  

^a Syst Simulation Dvmt Directorate   (United States)

^b NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CORRELATION METHODS; DATABASE SYSTEMS; KINETIC ENERGY; MATHEMATICAL MODELS; REYNOLDS NUMBER; SPECIFIC HEAT; TURBULENT FLOW;

HYPERSONIC FLOWS; RAPID ENGINEERING; TRANSPORT MODEL; TURBULENT TRANSITIONAL FLOWS;

HYPERSONIC AERODYNAMICS;

EID: 20844462435     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.1854     Document Type: Article

References (37)

1. Chang, Chau-Lyan, "The Langley Stability and Transition Analysis Code (LASTRAC): LST, Linear & Nonlinear PSE for 2-D Axisymmetric, and Infinite Swept Wing Boundary Layers," AIAA Paper 2003-0974, Jan. 2003.
2. So, R. M. C., Sarkar, S., Gerodimos, G., and Zhang, J., "A Dissipation Rate Equation for Low-Reynolds-Number and Near-Wall Turbulence," Theoretical Computational Fluid Dynamics, Vol. 9, Jan. 1997, pp. 47-63.
3. Chien, K.-Y., "Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model," AIAA Journal, Vol. 20, No. 1, 1982, pp. 33-38.
4. So, R. M. C., Zhang, H. S., and Speziale, C. G., "Near-Wall Modeling of the Dissipation Rate Equation" AIAA Journal, Vol. 29, No. 12, 1991, pp. 2069-2076.
5. Papp, J. L., and Dash, S. M., "Turbulence Model Unification and Assessment for High-Speed Aeropropulsive Flows," AIAA Paper 2001-0880, Jan. 2001.
6. Sarkar, S., "The Pressure-Dilatation Correlation in Compressible Flows," Physics of Fluids A, Vol. 4, No. 12, 1992, pp. 2674-2682.
7. Zeman, O., "Dilatation Dissipation: The Concept and Application in Modeling Compressible Mixing Layers," Physics of Fluids A, Vol. 2, No. 2, 1990, pp. 178-188.
8. Zeman, O., "On the Decay of Compressible Isotropic Turbulence," Physics of Fluids A, Vol. 3, No. 5, 1991, pp. 951-955.
9. Berkowitz, A. M., Kyriss, C. L., and Martellucci, A., "Boundary Layer Transition Flight Test Observations," AIAA Paper 77-125, Jan. 1977.
10. Warren, E. S., Harris, J. E., and Hassan, H. A., "Transition Model for High-Speed Flow," AIAA Journal, Vol. 33, No. 8, 1995, pp. 1391-1397.
11. Mee, D. J., "Boundary Layer Transition Measurements in Hypervelocity Flows in a Shock Tunnel," AIAA Paper 2001-0208, Jan. 2001.
12. Holden, M. C., and Rodriguez, K., "Experimental Studies of Shock Wave/Wall-Jet Interaction in Hypersonic Flows," Calspan-UB Research Center, Rept. 2610-1, Buffalo, NY, 1994.
13. Holden, M. C., "Studies of Scramjet Performance in the LENS Facilities," AIAA Paper 2000-3604, July 2000.
14. Schneider, S. P., "Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition," Journal of Spacecraft and Rockets, Vol. 38, No. 3, 2001, pp. 323-333.
15. Goyne, C. P., "Skin Friction Measurements in High Enthalpy Flows at High Mach Number," Ph.D. Dissertation, Dept. of Mechanical Engineering, Univ. of Queensland, Brisbane, Australia, 1999.
16. York, B. J., Kenzakowski, D. C., Lee, R. A., and Dash, S. M., "Upgrades to CRAFT Code for Simulation of Ducted Launcher/Plume Interactions," 1997 JANNAF EPTS & SPIRITS Users Group Joint Meeting, Lockheed Martin, Sunnyvale, CA, April 1997.
17. Thompson, J. F., Warsi, Z. U. A., and Mastin, C. W., Numerical Grid Generation: Foundation and Applications, North-Holland, New York, 1985.
18. Dhawan, S., and Narasimha, R., "Some Properties of Boundary Layer During the Transition from Laminar to Turbulent Flow Motion," Journal of Fluid Mechanics, Vol. 3, 1958, pp. 418-436.
19. Mayle, R., "The Role of Laminar Turbulent Transition in Gas Turbine Engines," Journal of Turbomachinery, Vol. 113, 1991, pp. 509-537.
20. Steelant, J., and Dick, E., "Modelling of Bypass Transition with Conditioned Navier-Stokes Equations Coupled to an Intermittency Transport Equation," International Journal for Numerical Methods in Fluids, Vol. 23, 1996, pp. 193-220.
21. Warren, E. S., and Hassan, H.A., "Transition Closure Model for Predicting Transition Onset," Journal of Aircraft, Vol. 35, No. 5, 1998, pp. 769-775.
22. n Method for Determining Set of Transition," AIAA Paper 97-0825, Jan. 1997.
23. Obremski, H. J., Morkovin, M. V., and Landahl, M., "Portfolio of Stability Characteristics of Incompressible Boundary Layer," AGARDograph 134, March 1969.
24. Walker, G. J., "Transitional Flow on Axial Turbomachine Blading" AIAA Journal, Vol. 27, No. 5, 1989, pp. 595-602.
25. Mack, L. M., "Linear Stability Theory and the Problem of Supersonic Boundary-Layer Transition," AIAA Journal, Vol. 13, No. 3, 1975, pp. 278-289.
26. Stetson, K. F., and Kimmel, R. L., "On Hypersonic Boundary Layer Stability," AIAA Paper 92-0737, Jan. 1992.
27. McDaniel, R. D., and Hassan, H. A., "Role of Bypass Transition in Conventional Hypersonic Facilities," AIAA Paper 2001-0209, Jan. 2001.
28. McDaniel, R. D., and Hassan, H. A., "Study of Bypass Transition Using the k-z Framework," AIAA Paper 2001-2310, June 2000.
29. Eckert, E. R. G., "Engineering Relations for Heat Transfer and Friction in High-Velocity Laminar and Turbulent Boundary Layer Flow over Surfaces with Constant Pressure and Temperature," Transactions of the American Society of Mechanical Engineers, Vol. 78, No. 6, 1956, p. 1273.
30. Schubauer, G. B., and Klebanoff, P. S., "Contributions on the Mechanics of Boundary-Layer Transition," NACA Rept. 1289, March 1956.
31. Schubauer, G. B., and Skramstad, H. K., "Laminar Boundary Layer Oscillations and Transition on a Flat Plate," NACA Rept. 909, 1948.
32. Savill, A. M., "Some Recent Progress in The Turbulence Modeling of Bypass Transition," Near-Wall Turbulent Flows, edited by R. M. C. So, C. G. Speziale, and B. E. Launder, Elsevier, Amsterdam, 1993, pp. 829-848.
33. Savill, A. M., "Further Progress in The Turbulence Modeling of Bypass Transition," Engineering Turbulence Modeling and Experiments 2, edited by W. Rodi and F. Martelli, Elsevier, Amsterdam, 1993, pp. 583-592.
34. He, Y., and Morgan, R. G., "Transition of Compressible High Enthalpy Boundary Layer Flow over a Flat Plate," Aeronautical Journal, Vol. 98, No. 972, 1994, pp. 25-34.
35. Wright, R. L., and Zoby, E. V., "Flight Boundary-Layer Transition Measurements on Slender Cone at Mach 20, " AIAA Paper 77-719, June 1977.
36. Wurster, K. E., Zoby, E. V., and Thompson, R. A., "Flowfield and Vehicle Parameter Influenc on Results of Engineering Aerothermal Methods," Journal of Spacecraft and Rockets, Vol. 28, No. 1, 1991, pp. 16-22.
37. Howard, F. G., "Thermal Analysis Methods and Bassic Heat Transfer Data for a Turbulent Heating Flight Experiment at Mach 20 (Reentry F)," NASA TMX-2282, March 1971.