Evaluation of ablation and longitudinal vortices in solid rocket motor by computational fluid dynamics

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 11, Issue , 2006, Pages 8832-8843

  Daimon, Yu ^a,c,d   Shimada, Toru ^a,c,d   Tsuboi, Nobuyuki ^a,c,d   Takaki, Ryoji ^a,e   Fujita, Kazuhisa ^a,f   Takekawa, Kuniyuki ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Institute of Space and Astronautical Science   (Japan)

^c Department of Space Transportation Engineering ^*  (Japan)

^d AIAA   (United States)

^e Center for Planning and Information Systems   (Japan)

^f Gasdynamics Research Group

Author keywords

[No Author keywords available]

Indexed keywords

CORRELATION EQUATION; SOLID ROCKET MOTOR; SURFACE RECESSION RATE;

ABLATION; NOZZLES; NUMERICAL METHODS; ROCKET ENGINES; SOLID PROPELLANTS; SURFACE TREATMENT;

COMPUTATIONAL FLUID DYNAMICS;

EID: 34249326906     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. Scchneider, P. J., Dolton, T. A., and Reed, G. W., "Mechanical Erosion of Charring Ablators in Ground-Test and Re-Entry Environments", AIAA Journal, Vol. 6, No. 1, 1968.
3. Larson, H. K. and Matter, G. G., "Cross-Hatching - A Coupling of Gas Dynamics with the Ablation Process", AIAA Paper 68-670, AIAA Fluid and Plasma Dynamics Conference, 1968.
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7. Baldwin, B. S. and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows", AIAA Paper 78-254, 1978.
8. Degani, D. and Schiff, L. B., "Computation of Turbulent Supersonic Flows around Pointed Bodies Having Cross flow Separation", Journal of Computational Physics, 66, pp.173-196, 1986.
9. Hopkins, E. J., Keating, K. Jr., and Bandettini, A., "Photographic Evidence of Streamwise Arrays of Vortice in Boundary-Layer Flow", NASA TN-D 328, 1960.
10. Ginoux, J. J., "Streamwise Vortices in Reattaching High-Speed Flows: A Suggested Approach", AIAA J., Vol. 9, No. 4, 759-560, 1971.