Effective calculation of multiphase flow fields in liquid rocket thrust chambers

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

  Wennerberg, Dag ^a   Knab, Oliver ^b  

^a Tecosim GmbH   (Germany)

^b AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; FLOW FIELDS; LIQUID FILMS; MULTIPHASE FLOW; PROPULSION; ROCKETS;

GRID REFINEMENT; GRID-INDEPENDENT SOLUTIONS; HIGH ASPECT RATIO; LIQUID ROCKETS; LOCAL GRID REFINEMENT; NEAR-WALL REGION; REGENERATIVELY COOLED; ROCKET THRUST;

ENGINES;

EID: 85086489719     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3407     Document Type: Conference Paper

References (3)

1. Preclik, D., Estublier, D., and Wennerberg, D., "An Eularian- Lagrangian Approach to Spray Combustion Modelling for Liquid Bi- Propellant Rocket Motors," 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Al A A 95-2779, Jul 1995.
2. Knab, O., Preclik, D., and Estublier, D., "Flow Field Prediction within Liquid Film Cooled Combustion Chambers of Storable Bi- Propellant Rocket Engines," 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA 98-3370, Jul 1998.
3. Knab, O, Frohlich, A, and Wennerberg, D. "Design Support for Advanced Storable Propellant Engines by ROCFLAM Analysis," 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 99-2459, Jim 1999.