Steady, subsonic CFD analysis of the VFE-2 configuration and comparison to wind tunnel data

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Crippa, Simone ^a   Rizzi, Arthur ^a  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC SIGNAL PROCESSING; DELTA WING AIRCRAFT; REYNOLDS NUMBER; VORTEX FLOW; WIND TUNNELS; WINGS;

BLUNT LEADING EDGES; COMPUTATIONAL RESULTS; FLOW EXPERIMENTS; NUMERICAL RESULTS; SURFACE FLOW PATTERNS; SURFACE PRESSURE COEFFICIENTS; VORTICAL STRUCTURES; WIND-TUNNEL DATA;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78149456322     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-397     Document Type: Conference Paper

References (20)

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