Numerical flowfield analysis of the next generation vulcan nozzle

Journal of Propulsion and Power

Volumn 12, Issue 4, 1996, Pages 655-661

  Hagemann, G ^a,c   Krulle G ^a,c   Hannemann, K ^b,d  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b Inst of Fluid Mechanics   (Germany)

^c Lampoldshausen Research Center

^d Heart Center   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; HYDROGEN; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; NOZZLES; NUMERICAL ANALYSIS; NUMERICAL METHODS; OXYGEN; THREE DIMENSIONAL; TURBULENT FLOW; VISCOUS FLOW;

CONSERVATION LAW; VULCAN ENGINE; VULCAN NOZZLE;

ROCKET ENGINES;

EID: 0030190391     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24086     Document Type: Article

References (9)

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2. Nickerson, G. R., Dang, L. D., and Coats, D. E., "Two-Dimensional Reference Computer Program," Marshall Space Flight Center, NAS 8-35931, Huntsville, AL, 1985.
3. Manski, D., and Hagemann, G., "Influence of Rocket Design Parameters on Engine Nozzle Efficiencies," AIAA Paper 94-2756, June 1994.
4. Anderson, J. D., Modem Compressible Flow, McGraw-Hill, New York, 1982.
5. Hagemann, G., Hannemann, K., and Krülle, G., "Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle," AIAA Paper 95-2782, July 1995.
6. Brossel, P., and Eury, S., "Development Status of Vulcain Engine and Its Upgraded Version Vulcain Mark II," International Astronautical Federation 94-S.2.411, 1994.
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8. Hagemann, G., "Supersonic Flows in Complex Nozzle Configurations of High-Performance Rocket Engines," DLR-FB 95-40, May 1996.
9. Popp, M., "A Study of Advanced Nozzle Technologies," ELITE Program, ESTEC Noordwijk, Oct. 1993.