Critical assessment of dual-bell nozzles

Journal of Propulsion and Power

Volumn 15, Issue 1, 1999, Pages 137-143

  Frey, Manuel ^a   Hagemann, Gerald ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; TRANSITION FLOW; WALL FLOW;

DUAL BELL NOZZLES; FLOW TRANSIENTS; WALL INFLECTION;

NOZZLES;

EID: 0032778224     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5402     Document Type: Article

References (10)

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3. Immich, H., and Caporicci, M., "FESTIP Technology Developments in Liquid Rocket Propulsion for Reusable Launch Vehicles," AIAA Paper 97-3311, 1997.
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9. Hagemann, G., Schley, C.-A., Odintsov, E., and Sobatchkine, A., 10 Nozzle Flowfield Analysis with Particular Regard to 3D-Plug-Cluster Configurations," AIAA Paper 96-2954, 1996.
10. Nickerson, G., Dang, L., and Coats, D., Two Dimensional Reference Computer Program, NAS 9-12652, NASA Marshall Space Flight Center, AL, April 1973.