Pitch rate and reynolds number effects on unsteady boundary-layer transition and separation

Journal of Aircraft

Volumn 35, Issue 1, 1998, Pages 46-52

  Schreck, Scott J ^a,d,f   Faller, William E ^b,e,f   Helin, Hank E ^c,d,f  

^a AIR FORCE OFFICE OF SCIENTIFIC RESEARCH   (United States)

^b JOHNS HOPKINS UNIVERSITY   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d Department of Mechanical Engineering ^*  (United States)

^e Department of Mechanical Engineering

^f AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; NUMERICAL ANALYSIS; REYNOLDS NUMBER; SHEAR STRESS; STRESS ANALYSIS; TRANSITION FLOW; UNSTEADY FLOW; VORTEX FLOW;

DYNAMIC STALL; PITCH RATE; SEPARATED FLOW;

AIRFOILS;

EID: 0031655088     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2258     Document Type: Article

References (18)

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