Effect of evaporating droplets on shock wave attenuation

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Kersey, James ^a   Loth, Eric ^a   Lankford, Dennis ^b  

^a University of Illinois at Urbana Champaign   (United States)

^b Aerospace Testing Alliance   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTICAL SOLUTIONS; AXIAL LOCATIONS; CONTINUOUS PHASE; COUPLING EFFECT; DROPLET MASS; DROPLET SIZES; ENERGY COUPLINGS; EVAPORATION AND CONDENSATION; EVAPORATION RATE; GAS FLOWS; GAS TEMPERATURE; INTERPHASE TRANSFER; KNUDSEN NUMBERS; LAGRANGIAN FORMULATIONS; MASS LOADINGS; NON EQUILIBRIUM; NUMERICAL RESULTS; SHOCK ATTENUATION; SHOCK STRENGTH; SHOCK WAVE ATTENUATIONS; SIMULATION CAPABILITY; SMALL-DIAMETER; SPECIFIC HEAT RATIO; THERMAL LOADINGS; UNSTRUCTURED GRID; VELOCITY CHANGES;

AERODYNAMICS; AEROSPACE ENGINEERING; DRAG; DROP FORMATION; HEAT TRANSFER; LOADING; MACH NUMBER; SHOCK WAVES; SPECIFIC HEAT; THERMAL EVAPORATION; THERMAL STRESS;

GASES;

EID: 77957114629     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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