Loosely coupled simulation for Two-dimensional ablation and shape change

5th AIAA Theoretical Fluid Mechanics Conference

Volumn , Issue , 2008, Pages

  Chen, Yih Kanq ^a   Milos, Frank S ^a   Gökçen, Tahir ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b ELORET CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

A-THERMAL; ANGLES OF ATTACK; COUPLED SIMULATION; DATA PARALLEL; FLOW SOLVER; GOVERNING EQUATIONS; HIGH FIDELITY; LOOSE COUPLINGS; MATERIAL RESPONSE; NON EQUILIBRIUM; SHAPE CHANGE; SURFACE ENERGY BALANCE; SURFACE HEAT FLUXES; SURFACE RECESSION; TEST MODELS; THERMAL PROTECTION SYSTEM; THERMAL RESPONSE; THREE-COMPONENT; TIME-ACCURATE;

ABLATION; CONTACTS (FLUID MECHANICS); FLUID MECHANICS; HEAT FLUX; HEAT SHIELDING; SURFACE CHEMISTRY; SURFACES; THERMAL INSULATING MATERIALS; TWO DIMENSIONAL;

NAVIER STOKES EQUATIONS;

EID: 78049303625     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Tran, H., Johnson, C, Rasky, D., Hui, F., Chen, Y.-K., and Hsu, M., "Phenolic Impregnated Carbon Ablators (PICA) for Discovery Class Missions, " AIAA Paper 96-1911, June 1996.
2. Willcockson, W.H,. "Stardust Sample Return Capsule Design Experience, " Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 470-474.
3. Chen, Y.-K., and Milos, F.S., "Multi-Dimensional Effects on Heatshield Thermal Response for the Orion Crew Module, " AIAA Paper 2007-4397, 39th AIAA Thermophysics Conference, June 2007.
4. Milos, F.S. and Chen, Y.-K., "Two-Dimensional Ablation, Thermal Response, and Sizing Program for Pyrolyzing Ablators, " AIAA Paper 2008-1223, AIAA Aerospace Sciences Meeting and Exhibition, January 2008, Reno, NV.
5. Chen, Y.-K., and Milos, F.S., "Ablation and Thermal Analysis Program for Spacecraft Heatshield Analysis, " Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 475-483.
6. Moyer, C.B., and Rindal, R.A., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part II, Finite Difference Solution for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances, " NASA CR-1061, 1968.
7. Chen, Y.-K., and Milos, F.S., "Two-Dimensional Implicit Thermal Response and Ablation Program for Charring, " Journal of Spacecraft and Rockets, Vol. 38, No. 4, 2001, pp. 473-481.
8. Rafinejad, D, Dahm, T.J., Brink, D.F., Abbett, M.J., and Wolf, C.J., "Passive Nosetip Technology (PANT II) Program Volume II. Computer User's Manual: ABRES Shape Change Code (ASCC), " Report SAMSO-TR-77-11, October 1976.
9. Candler, G.V., and MacCormack, R.W., "Computation of Weakly Ionized Hypersonic Flows in Thermochemical Nonequilibrium, " Journal of Thermophysics and Heat Transfer, Vol. 5, No. 3, 1991, pp. 266-273.
10. Dahm, T.J., Cooper, L., Rafinejad, D., Youngblood, S.B., and Kelly, J.T., "Passive Nosetip Technology (PANT II) Program Volume I. Inviscid Flow and Heat Transfer Modeling for Reentry Vehicle Nosetips, " Report SAMSO-TR-77-11, October 1976.
11. 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.
12. Chen, Y.-K., and Milos, F.S., "Three-Dimensional Ablation and Thermal Response Simulation System, " AIAA Paper 2005- 5064, June 2005.
13. Squire, T.H., Milos, F.S., Hartlieb, G.C., and Rasky, D.J., "TPSX: Thermal Protection Systems Expert and Material Property Database, " ICCE Fourth International Conference on Composites Engineering, ICCE and College of Engineering, University of New Orleans, July 1997, pp. 937-938.
14. Kendall, R.M., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part V, A General Approach to the Thermochemical Solution of Mixed Equilibrium-Nonequilibrium Homogeneous or Heterogeneous Systems, " NASA CR-1064, 1968.
15. Milos, F.S., and Chen, Y.-K., "Comprehensive Model for Multi-Component Ablation Thermochemistry, " AIAA Paper 97- 0141, 1997.
16. Covington, M.A., Heinenmann, J.M., Goldstein, H.E., Chen, Y.-K., Terrazas-Salinas, I., Balboni, J.A., Olejniczak, J., and Martinez, E.R., "Performance of a Low Density Ablative Heat Shield Material, " Journal of Spacecraft and Rockets, Vol. 45, No. 2, 2008, pp. 237-247.