Tunnel wall effect on the flow around a 76/40-deg double-delta wing

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Verhaagen, N G ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; VORTEX FLOW; WIND TUNNELS; WINGS;

AERODYNAMIC CHARACTERISTICS; CORRECTION METHOD; DOUBLE-DELTA WINGS; EXISTING TUNNEL; LEADING-EDGE VORTICES; NUMERICAL SOLUTION; SUBSONIC WIND TUNNELS; SURFACE PRESSURES;

DELTA WING AIRCRAFT;

EID: 84983134833     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-312     Document Type: Conference Paper

References (23)

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