SSME fuel preburner phase 1/phase 2+ comparison

Book · Tue Jan 01 00:00:00 EST 1985

OSTI ID:6994482

Jensen, R J; Liang, P Y; Pinkowski, S M

An analytical comparison of the predicted combustion flowfields for the Phase 1 and Phase 2+ fuel preburner configurations using an advanced CFD combustion code is currently underway at Rocketdyne. The Phase 2+ injector has a modified element design. The redesigned element provides for improved atomization through a shift in the injector element/face bleed flow split while maintaining an acceptable pressure drop. Cold-flow tests of the new design have been encouraging. As a complement to those tests, the Advanced Rocket Injector Combustor Code (ARICC) was selected to conduct a detailed combustion flowfield simulation. ARICC models two-dimensional (or axisymmetric), transient, turbulent, two-phase mixing and combustion flowfields. It is derived from a member of the Los Alamos ICEd-ALE family of codes. Unique features of ARICC include explicit representation of the coaxial LOX jet and hydrogen gas flows, distributed atomization processes, droplet breakup, and supercritical vaporation processes. Predictions of temperature and OH concentration profiles for the Phase 1 and Phase 2+ injector flowfields indicate a trend toward more uniform temperature distributions and shorter flame lengths with the Phase 2+ design.

• OSTI ID: 6994482
• Country of Publication: United States
• Language: English

Related Subjects

37 INORGANIC
ORGANIC
PHYSICAL AND ANALYTICAL CHEMISTRY
42 ENGINEERING
FUEL INJECTION SYSTEMS
COMPUTERIZED SIMULATION
ATOMIZATION
COMBUSTION KINETICS
COMPARATIVE EVALUATIONS
FLAMES
GAS FLOW
HYDROGEN
TEMPERATURE DISTRIBUTION
CHEMICAL REACTION KINETICS
ELEMENTS
FLUID FLOW
FUEL SYSTEMS
KINETICS
NONMETALS
REACTION KINETICS
SIMULATION
400800* - Combustion
Pyrolysis
& High-Temperature Chemistry
421000 - Engineering- Combustion Systems