Design of a double diaphragm shock tube for fluid disintegration studies

Review of Scientific Instruments

Volumn 79, Issue 12, 2008, Pages

  Stotz, Ingo ^a   Lamanna, Grazia ^a   Hettrich, Harald ^a   Weigand, Bernhard ^a   Steelant, Johan ^b  

^a UNIVERSITY OF STUTTGART   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; CONTROL SYSTEMS; DIAPHRAGMS; FLOW VISUALIZATION; FLUID DYNAMICS; HYDRODYNAMICS; SHOCK TUBES; SHOCK WAVES; TUBES (COMPONENTS);

BOUNDARY LAYER EFFECTS; ELEVATED PRESSURES; ENGINE CONDITIONS; FILLING SYSTEMS; FUNDAMENTAL PROCESSES; INJECTION CONDITIONS; QUALIFICATION TESTS; REFLECTED SHOCKS; REPRODUCIBILITY; REPRODUCIBLE TESTS; SET-UPS; SHOCK ATTENUATIONS; SHOCK TUBE FACILITIES; SPECIAL FEATURES; SPRAY ATOMIZATIONS; TEST CONDITIONS; TEST SECTIONS; TEST TIMES;

TESTING;

EID: 58149260841     PISSN: 00346748     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.3058609     Document Type: Article

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