Computational/Experimental aeroheating predictions for X-33 phase II vehicle

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Hamilton, H Harris ^a   Weilmuenster, K James ^a   Horvath, Thomas J ^a   Berry, Scott A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; CODES (SYMBOLS); HEATING RATE; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; TURBULENT FLOW; VEHICLES; WIND TUNNELS;

ANGLES OF ATTACK; CIRCUMFERENTIAL DIRECTION; LAMINAR AND TURBULENT FLOW; NAVIER-STOKES CODE; TRANSITION-TO-TURBULENT FLOWS; TURBULENT HEATING; WIND-TUNNEL DATA; WINDWARD SURFACE;

HEATING;

EID: 84983195564     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (25)

1. Bekey, I., Powell, R., and Austin, R., "NASA Studies Access to Space," Aerospace America, May 1994, pp. 38-43.
2. Cook, S. A., "X-33 Reusable Launch Vehicle Structural Technologies," AIAA Paper 97-10873, Nov. 1996.
3. Freeman Jr., D. C., Talay, T. A., and Austin, R. B., "Reusable Launch Vehicle Technology Program," AIAA Paper IAF 96-V. 4. 01, Oct. 1996.
4. Rodi, P., Green, M. G., and Zoby, E. V., "An Overview of the Aerothermal Design of the X-33 Vehicle," AIAA Paper 98-0863, Jan. 1998.
5. Thompson, R. A., Hamilton II, H. H., Berry, S. A., Horvath, T. J., and Nowak, R. W., "Hypersonic Boundary Layer Transition for X-33 Phase II Vehicle," AIAA Paper 98-0867, Jan. 1998.
6. Micol, J. R., "Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center: Aerothermodynamic Facilities Complex," AIAA Paper 95-2107, Jun. 1995.
7. Buck, G. M., "Automated Thermal Mapping Techniques Using Chromatic Image Analysis," NASA TM 101554, Apr. 1989.
8. Merski, Jr., N. R., "Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package," AIAA Paper 98-00712, Jan. 1998.
9. Buck, G. M. and Vasquez, P., "An Investment Ceramic Slip-Casting Technique for Net-Form, Precision, Detailed Casting of Ceramic Models," U. S. Pattent 5266252, Nov. 1993.
10. Micol, J. R., "Aerothermodynamic Measurement and Prediction for a Modified Orbiter at Mach 6 and 10 in Air," AIAA Paper 91-1436, Jun. 1991.
11. Gnoffo, P. A., "An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous, Compressible Perfect-Gas Flows," NASA TP 2953, Feb. 1990.
12. Gnoffo, P. A., "Point-Implicit Relaxation Strategies for Viscous, Hypersonic Flows," Computational Methods in Hypersonic Aerothermodynamics, edited by T. K. S. Murthy, Computational Mechanics Publications, Kluwer Academic Publishers, 1991, pp. 115-151.
13. Cheatwood, F. M. and Gnoffo, P. A., "Users Manual for the Langley Aerthermodynamic Upwind Relaxation Algorithm (LAURA)," NASA TM 4674, Apr. 1996.
14. Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Oct. 1981, pp. 357-372.
15. Yee, H. C., "On Symmetric and upwind TVD Schemes," NASA TM 88325, 1990.
16. Gnoffo, P. A., Weilmuenster, K. J., and Alter, S. J., "Multiblock Analysis for Shuttle Orbiter Re-Entry Heating from Mach 24 to Mach 12," Journal of Spacecraft and Rockets, May-Jun. 1994, pp. 367-377.
17. Gnoffo, P. A., "Code Calibration Program in Support of the Aeroassist Flight Experiment," Journal of Spacecraft and Rockets, Mar.-Apr. 1990, pp. 131-142.
18. Hamilton, II, H. H., DeJarnette, F. R., and Weilmuen-ster, K. J., "Application of Axisymmetric Analog for Calculating Heating in Three-Dimensional Flows," Journal of Spacecraft and Rockets, Vol. 24, Jul.-Aug. 1987, pp. 296-302.
19. Hamilton II, H. H., Greene, F. A., and DeJarnette, F. R., "Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles," Journal of Spacecraft and Rockets, Vol. 31, No. 3, May-Jun. 1994, pp. 345-354.
20. Cooke, J. C., "An Axially Symmetric Analogue for General Three-Dimensional Boundary Layers," Reports and Memoranda 3200, 1961.
21. Zoby, E. V., Moss, J. N., and K., S., "Approximate Convective Heating Analysis for Hypersonic Flows," Journal of Spacecraft and Rockets, Vol. 18, No. 1, Jan. 1981, pp. 64-70.
22. Candler, G. V., Wright, M. J., and McDonald, J. D., "Data-Parallel Lower-Upper Relaxation Method for Reacting Flows," AIAA Journal, Vol. 32, No. 12, Dec. 1994, pp. 2380-2386.
23. Riley, C. J., Kleb, W. L. K., and Alter, S. J., "Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method," AIAA Paper 98-0880, Jan. 1998.
24. Fay, J. A. and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," Journal of the Aeronautical Sciences, Vol. 25, No. 2, Feb. 1958, pp. 73-85.
25. Berry, S. A., Bouslog, S. A., Brauckmann, G. J., and Caram, J. M., "Boundary Layer Transition Due to Isolated Roughness: Shuttle Results from LaRC 20-Inch Mach 6 Tunnel," AIAA Paper 97-0273, Jan. 1997.