Airfoil boundary-layer development and transition with large leading-edge roughness

AIAA Journal

Volumn 35, Issue 1, 1997, Pages 75-84

  Kerho, Michael F ^a,b,c   Bragg, Michael B ^a,b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b 306 Talbot Laboratory   (United States)

^c BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANEMOMETERS; BOUNDARY LAYERS; DENSITY OF GASES; FLOW MEASUREMENT; REYNOLDS NUMBER; SURFACE ROUGHNESS; TRANSITION FLOW; TURBULENCE; TURBULENT FLOW; ULTRASONIC VELOCITY MEASUREMENT;

FLOW FIELD INTERMITTENCY MEASUREMENT;

AERODYNAMICS;

AEROFOILS; BOUNDARY LAYERS; MODELLING-MATHEMATICAL;

EID: 0030888608     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.65     Document Type: Article

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