Effects of shear on ablation characteristics of charring low-temperature ablatives

34th Thermophysics Conference

Volumn , Issue , 2000, Pages

  Wong, J L ^a   Jovanovic, V ^a   Tang, I ^a   Broeren, R ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; AIRSHIPS; NASA; PHENOLIC RESINS; TEMPERATURE;

BOEING COMPANIES; CONVECTIVE HEATING; FLIGHT CONDITIONS; FLUX CONDITIONS; LINEAR DEPENDENCE; LOW TEMPERATURES; ST. LOUIS , MISSOURI; SURFACE CRACKING;

SHEAR FLOW;

EID: 85088718840     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-2436     Document Type: Conference Paper

References (13)

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3. Adams, M.C., "Recent Advances in Ablation, " ARS Journal, September 1959.
4. nd Aerospace Science Meeting, 65-117, New York, 1965.
5. th Thermophysics Conference, 7/92.
6. TPSX (Thermal Protection Systems Expert and Material Property Database), NASA Ames, Moffett Field, CA.
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11. Engel, C.D., "LANMIN User's Manual, " NASA CR 172212, Aug 1983.
12. Bertram, M. H., and Cook, B. S., "The Correlation of Oblique Shock Parameters for Ratios of Specific Heats from 1 to 5/3 with Applications to Real Gas Flows, " NASA TR R-171, 1963.
13. Marvin, J.G., and Pope, R.B., "Laminar Convective Heating and Ablation in Mars Atmosphere, " J. AIAA, vol. 5, no 2, 1967.