Experimental study of the nozzle surface regression rate to the heat transfer

Journal of Propulsion and Power

Volumn 22, Issue 1, 2006, Pages 221-223

  Lee, Tae Ho ^a,b  

^a Agency for Defence Development   (South Korea)

^b Propulsion Department   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; HEAT TRANSFER; PRESSURE EFFECTS; RAW MATERIALS; SURFACE PHENOMENA; THERMAL INSULATING MATERIALS;

CONVECTIVE HEAT TRANSFER; FIRST-ORDER POLYNOMIALS; HEAT TRANSFER COEFFICIENT; THERMAL INSULATORS;

NOZZLES;

EID: 32844458461     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.12341     Document Type: Article

References (8)

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3. Schneider, P. J., Dolton, T. A., and Reed, G. W., "Mechanical Erosion of Charring Ablators in Grounds Test and Re-Entry Environments," AIAA Journal, Vol. 6, No. 1, 1968, pp. 64-72.
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7. Gowariker, V. R., "Mechanical and Chemical Contributions to the Erosion Rates of Graphite Throats in Rocket Motor Nozzles," Journal of Spacecraft and Rockets, Vol. 3, No. 10, 1966, pp. 1490-1494.
8. Kays, W. M., and Crawford, M. E., "Convective Heat Transfer at High Velocities," Convective Heat and Mass Transfer, 2nd ed., McGraw-Hill, New York, 1980, pp. 300-310.