Sharp refractory composite leading edges on hypersonic vehicles

12th AIAA International Space Planes and Hypersonic Systems and Technologies

Volumn , Issue , 2003, Pages

  Walker, Sandra P ^a   Sullivan, Brian J ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Materials Research & Design   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE ELEMENT METHOD; HEATING; REFRACTORY MATERIALS; SHOCK PROBLEMS; THERMAL SHOCK;

AIR BREATHING VEHICLES; COMPOSITE MATERIAL SYSTEM; DESIGN DEVELOPMENT; FIBER ARCHITECTURE; MATERIAL SYSTEMS; REFRACTORY COMPOSITES; STRUCTURAL FINITE ELEMENTS; STRUCTURAL RESPONSE;

HYPERSONIC VEHICLES;

EID: 85087601753     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-6915     Document Type: Conference Paper

References (9)

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3. st Annual Conference on Composites, Materials and Structures, Cocoa Beach, FL, January 1997.
4. J. Spain and S. Starrett, Mechanical and Thermal Evaluation of Coated Carbon-Carbon, Southern Research Institute Final Report to General Dynamics Fort Worth Division, SRI-ME- 91-271-6913, April 1991.
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6. N.J. Pagano and G.P. Tandon, Elastic Response of Multidirectional Coated Fiber Composites, Composites Science and Technology, Vol. 31, 1988, 273-293.
7. B.W. Rosen, et al., An Analysis Model for Spatially Oriented Fiber Composites, Composite Materials Testing and Design, ASTM STP 617, 1977, pp. 243-259.
8. Lidman, W.G. and Bobrowsky, A. R., Correlation of Physical Properties of Ceramic Materials with Resistance to Fracture by Thermal Shock, NACA TN 1918, July 1949.
9. Wang, Y. R. and Chou, T. W., Thermal Shock Resistance of Laminated Ceramic Matrix Composites, Journal of Material Science, 26, 1991, pp. 2961-2966.