Validation of an Aerothermochemical Model for Graphite Nozzle Recession and Heat-Transfer Processes

References

• Back , L. H. , and Cuffel , R. F. ( 1970 ) Relationship between temperature and velocity profiles in a turbulent boundary layer along a supersonic nozzle with heat transfer . AIAA Journal 8 ( 11 ), Nov. 1970 , 2066 .
   Web of Science ®Google Scholar
• Cvelbar , D. A. ( 1981 ) Nozzle recession study. Presented at the 1981 JANNAF Propulsion Meeting , New Orleans , LA , May 1981 . CPlA Publication 342 , pp. 51 – 68 .
   Google Scholar
• Dirling , R. B. Jr. , Heightland , C. N. , Loomis , W. C. , Ellis , R. A. , and Kearney , A. J. ( 1983 ). Composite material analysis . Technical Report AFWAL-TR-83-4082, Oct. 1983 .
   Google Scholar
• Geisler , R. L. ( 1981 ). The prediction of graphite rocket nozzle recession rates. Presented at the 1981 JANNAF Propulsion Meeting , New Orleans , LA , May 1981 . CPIA Publication 342 pp. 173 – 196 .
   Google Scholar
• Gordon , S. , and McBride , B. J. ( 1976 ). Computer program for calculation of complex chemical equilibrium compositions, rockct performance incident and reflected shocks, and Chapman-Jouguet detonations . NASA-SP-273, 1976 .
   Google Scholar
• Keswani , S. T. , and Kuo , K. K. ( 1983 ). An aerothermochemical model of carbon-carbon composite nozzle recession . Proceedings of AIAA/ASME/ASCE/AHS Twenty-Fourth Structures, Structural Dynamies and Materials Conference , May 1983 , Lake Tahne , NE , pp. 348 – 358 .
   Google Scholar
• Keswani , S. T. , Andiroglu , E. , Campbell , J. D. , and Kuo , K. K. ( 1985 ) Recession behavior of graphitic nozzles in simulated rocket motors . Presented at the 19th AIAA/SAE/ASME Joint Propulsion Conference , June 1983 , Seattle , Washington . ( To be published in Journal of Spacecraft and Rackets, 1985 ).
   Google Scholar
• Khitrin , L. N. ( 1956 ). Fundamental principles of carbon combustion and factors intensifying the burning of solid fuels . Sixth Symposium on Combustion , pp. 565 – 573 .
   Google Scholar
• King , M. K. ( 1971 ). Kinetics of high-temperature reactions of graphite with carbon dioxide and water . Journal of Spacecraft and Rockets 8 , 470 .
   Web of Science ®Google Scholar
• Klager , K. ( 1977 ). The interaction of the efflux of solid propellants with nozzle materials . Propellants and Explosives 2 , 55 .
   Web of Science ®Google Scholar
• Kuo , K. K. , and Keswani , S. T. ( 1985 ). A comprehensive theoretical model for carbon-carbon composite nozzle recession . Combustion Science and Technology 42 , 145 . ( Also CPlA Publication 367, Oct. 1982, pp. 243-257 ).
   Web of Science ®Google Scholar
• Lewis . J. C. , Floyd . I. J. , and Cowlard , F. C. ( 1970 ). A laboratory investigation of carbon-gas reactions of relevance to rocket nozzle erosion . AGARD Conference Proceedings No. 52 , Feb , 1970 .
   Google Scholar
• Libby , P. A. , and Blake , T. R. ( 1981 ). Burning carbon particles in the presence of water vapor . Combustion and Flame 41 , 123 .
   Web of Science ®Google Scholar
• Swope , L. M. , and Berard , M. F. ( 1981 ). Effects of solid rocket formulation and exhaust gas chemistries on the erosion of graphite nozzles . Presented at AIAA Solid Propellant Rocket Conference , Jan , 1964 , Palo Alto , CA .
   Google Scholar
• Walker , P. L. , Rusinko , F. , and Austin , L. G. ( 1959 ). Gas reactions of carbon . Advances in Caralysts 11 . Academic Press , New York , pp. 133 – 221 .
   Google Scholar