Unsteady navier-stokes rocket nozzle flows

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Chang, I Shih ^a,d   Chang, Chau Lyan ^b,e   Chang, Sin Chung ^c,f  

^a AEROSPACE CORPORATION   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

^d Vehicle Systems Division   (United States)

^e Research and Technology Directorate   (United States)

^f Propulsion Systems Division

Author keywords

[No Author keywords available]

Indexed keywords

AMBIENT PRESSURES; ANALYSIS RESULTS; AXISYMMETRIC; CE/SE METHOD; CONVERGENT-DIVERGENT NOZZLE; DISTINCTIVE FEATURES; EXPERIMENTAL TEST; GLOBAL FLUX; HIGH ASPECT RATIO; INCIDENT SHOCK; MACH DISK; NAVIER STOKES; NEAR FIELDS; NOZZLE FLOW; REFLECTED SHOCKS; ROCKET NOZZLES; SHEAR LAYER; SOLUTION PROCEDURE; SPACE AND TIME; STEADY-STATE FLOWS; TRIANGULAR ELEMENTS; UNSTEADY ANALYSIS; UNSTRUCTURED MESHES; VISCOUS BOUNDARY LAYERS; VORTEX RINGS; WAVE INTERACTIONS;

ASPECT RATIO; ATMOSPHERIC THERMODYNAMICS; FLOW SEPARATION; MESH GENERATION; NAVIER STOKES EQUATIONS; PROPULSION; ROCKETS; TURBULENCE MODELS;

NOZZLES;

EID: 77957835850     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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