Diffuser design and performance analysis by unified integral methods

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Johnston, James P ^a  

^a Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; DUCTS; FIGHTER AIRCRAFT; PROPULSION;

COMPUTATIONAL TOOLS; FLOW DISTORTION; INLET BOUNDARY LAYER; INTEGRAL METHOD; PERFORMANCE ANALYSIS; PRELIMINARY DESIGN; PRESSURE RECOVERY; SUBSONIC DIFFUSERS;

DESIGN;

EID: 84962863570     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (48)

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