Orbiter gap filler bending model for re-entry

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 8, Issue , 2007, Pages 4977-4994

  Campbell, Charles H ^a,e,f   Driver, David M ^b,f,g   Alter, Stephen J ^c,f,h   Fasanella, Edwin L ^c,f,i   Wood, William A ^c,f,h   Stone, Jeffrey S ^d,j  

^a NASA JOHNSON SPACE CENTER   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d BOEING COMPANY   (United States)

^e Applied Aeroscience and CFD Branch   (United States)

^f AIAA   (United States)

^g Reacting Flow Branch   (United States)

^h M S 408A

ⁱ M S 495

^j Flight Sciences Aerodynamics

more..

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CERAMIC MATERIALS; FLIGHT DYNAMICS; HEAT TREATMENT; ORBITS; REENTRY; THERMAL STRESS;

AERODYNAMIC EFFECTS; CERAMIC GAP FILLERS; THERMAL PROTECTION SYSTEMS;

HEAT SHIELDING;

EID: 34347208680     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-413     Document Type: Conference Paper

References (24)

1. An, M. Y., Wang, K. C., Campbell, C. H., and Pelley, T. L., "Space Shuttle Orbiter Aerodynamics Induced by Asymmetric Boundary-Layer Transition", AIAA Paper 96-0808, January 1996.
2. Berry, S.A., Bouslog, S.A., Brauckmann, G.J., and Caram, J.M., "Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness," J. of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp. 241-248.
3. Bouslog, S.A., An, M.Y., and Deny, S.M., "Orbiter Windward Surface Boundary Layer Transition Flight Data," NASA CP-3248, Orbiter Experiments (OEX) Aerothermodynamics Symposium, April 1995, pp. 703-739.
4. Bouslog, S.A., Bertin, J.J., Berry, S.A., and Caram, J.M., "Isolated Roughness Induced Boundary-Layer Transition: Shuttle Orbiter Ground Tests and Flight Experience," AIAA Paper 97-0274, January 1997.
5. Bertin, J.J., and Stetson, K.F., "The Effect of Surface Roughness on Shuttle Orbiter Boundary-Layer Transition," Technical Report JSC-27358, NASA Johnson Space Center, January 1996.
6. Berry, S.A., "RTF BLT Task Peer Review: Disposition of Shuttle Orbiter TPS Damage or Repair from the Perspective of Hypersonic Boundary Layer Transition," Orbiter Entry Aeroheating Note 0305-017, March 2005.
7. Campbell, C. H., Anderson, B., Bourland, G., Bouslog, S. A., Cassady, A. M., Horvath, T. J., Berry, S. A., Gnoffo, P. A., Wood, W. A., Reuther, J., Driver, D., Chao, D., Hyatt, A.J., and Picetti, D., "Orbiter Return To Flight Entry Aeroheating," AIAA-2006-2917, June 2006.
8. Berry, S. A., Horvath, T. J., Greene, F. A., Kinder, G. R., and Wang, K.C., "Overview of Boundary Layer Transition Research in Support of Orbiter Return to Flight," AIAA-2006-2918, June 2006.
9. Horvath, T. J., Berry, S. A., Merski, N. R., Berger, K. T., Liechty, D. S., Buck, G. M., and Schneider, S. P., "Shuttle Damage/Repair From the Perspective of Hypersonic Boundary Layer Transition - Experimental Results," AIAA-2006-2919, June 2006.
10. Greene, F. A., and Hamilton, H., "Development of a Boundary Layer Properties Interpolation Tool in Support of Orbiter Return-To-Flight," AIAA-2006-2920, June 2006.
11. McGinley, C., Berry, S. A., Kinder, G. R., Barnwell, M., Wang, K. C., and Kirk, B. S., "Review of Orbiter Flight Boundary Layer Transition Data," AIAA-2006-2921, June 2006.
12. Berry, S. A., Horvath, T. J., Cassady, A. M., Kirk, B. S., Wang, K.C., and Hyatt, A. J., "Boundary Layer Transition Results From STS-114," AIAA-2006-2922, June 2006.
13. King, R., Kegerise, M., Berry, S. A., et. al, Currently unpublished Orbiter boundary layer testing results in NASA Langley Research Center Hypersonic Aerothermodynamics Complex.
14. Wadhams, T.P., Smolinski, G.J., Holden, M.S., and MacLean, M.G, "Experimental Space Shuttle Orbiter Studies to Acquire Data for Code and Flight Heating Model Validation," AIAA-2007-551, January 2007.
15. Cassady, A., Bourland, G., King, R., Kegerise, M., Berry, S. A., et. al, Currently unpublished Orbiter heating test MH-13 results at CUBRC.
16. Reuther, J.J., McDaniel, R.D., Brown, J., Prabhu, D., Saunders, D., and Palmer, G., "External Computational Aerothermodynamic Analysis of the Space Shuttle Orbiter at STS-107 Flight Conditions," AIAA 2004-2281, June 2004.
17. Pulsonetti, M. and Wood, W., "Computational Aerothermodynamics Assessment of Space Shuttle Orbiter Tile Damage - Open Cavities", AIAA 2005-4679, June 2005.
18. Alter, S.J., Reuther, J.J., and McDaniel, R.D., "Development of a Flexible Framework for Hypersonic Navier Stokes Space Shuttle Orbiter Meshes: Final Report," AIAA 2005-2635, June 2004.
19. Gnoffo, P.A., "An Upwind Biased Point Implicit Relaxation Algorithm for Viscous, Compressible Perfect Gas Flows," NASA TP 2953, February 1990.
20. Gnoffo, P.A., Gupta, R.N., and Shin, J.L., "Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium," NASA TP 2867.
21. Wright, M.J., Candler, G.V., and Bose, D., "Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp. 1603-1609.
22. "Equations, Tables, and Charts for Compressible Flow," NACA 1135, 1953.
23. Fasanella, E.L., "Ames Gap Filler Bend Test Results Final Report", internal NASA Langley Research Center memo, December 2006.
24. Carney, K., Moon, D.G., Fasanella, E.L., et. al, private communication of NASA Glenn Research Center static loading results on ceramic Ames gap fillers, March 2006.