Effects of flow separation on aerodynamic loads in linearized thin airfoil theory

Journal of Aircraft

Volumn 41, Issue 4, 2004, Pages 944-948

  Khrabrov, A ^a   Ol, M ^b,c  

^a CENTRAL AEROHYDRODYNAMIC INSTITUTE TSAGI   (Russian Federation)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Aeronautical Sciences Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; APPROXIMATION THEORY; BOUNDARY CONDITIONS; COMPUTER SIMULATION; CONFORMAL MAPPING; FUNCTIONS; IMAGE ANALYSIS; INTEGRAL EQUATIONS; PROBLEM SOLVING; VECTORS;

FLOW SEPARATION; IMAGE PLANES; PITCHING MOMENTS; POINT LOCATION;

AERODYNAMIC LOADS;

EID: 4344605857     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.5524     Document Type: Article

References (9)

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