Effect of tab parameters on near-field jet plume development

Journal of Propulsion and Power

Volumn 22, Issue 3, 2006, Pages 576-585

  Behrouzi, Parviz ^a,b   McGuirk, James J ^a,b  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

^b Department of Aeronautical and Automotive Engineering ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT PROPULSION; FLUORESCENCE; NOISE ABATEMENT; NOZZLES; SCHLIEREN SYSTEMS; SUBSONIC FLOW; THERMAL PLUMES; VORTEX FLOW;

AIRCRAFT DESIGN; JET NOISE REDUCTION; JET PLUME DEVELOPMENT; MACH NUMBER; TAB PARAMETERS; VELOCITY RATIO; VORTICITY;

JET ENGINES;

EID: 33744977030     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.15473     Document Type: Article

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