Development of vortex generator use for a transitioning high-speed inlet

Journal of Aircraft

Volumn 35, Issue 4, 1998, Pages 536-543

  Wendt, Bruce J ^a,c   Dudekt, Julianne C ^b,d,e  

^a Modern Technologies Corp   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c Aerospace Propulsion Division   (Switzerland)

^d Inlet Branch   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; DRAG; INTAKE SYSTEMS; NAVIER STOKES EQUATIONS; PRESSURE; VORTEX FLOW;

AIRCRAFT ENGINE INLET; PRESSURE RECOVERY; SUBSONIC DIFFUSER; VORTEX GENERATOR;

SUBSONIC AERODYNAMICS;

EID: 0032117162     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2357     Document Type: Article

References (19)

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