Transient two-dimensional analysis of side load in liquid rocket engine nozzles

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Wang, Ten See ^a,b  

^a NASA MARSHALL SPACE FLIGHT CENTER   (United States)

^b Applied Fluid Dynamics Analysis Group   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AFTERBURNERS (ENGINE); ASPECT RATIO; COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; PROPULSION; ROCKETS;

AXISYMMETRIC NOZZLES; COMPUTATIONAL METHODOLOGY; COMPUTATIONAL STRATEGY; LIQUID ROCKET ENGINES; NUMERICAL INVESTIGATIONS; RESTRICTED SHOCK SEPARATION; TWO-DIMENSIONAL ANALYSIS; TWO-DIMENSIONAL GEOMETRY;

ROCKET NOZZLES;

EID: 85086610692     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-3680     Document Type: Conference Paper

References (16)

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