Wind-tunnel interference effects on a 70° delta wing

Aeronautical Journal

Volumn 108, Issue 1088, 2004, Pages 505-513

  Allan, M R ^a   Badcock, K J ^a   Barakos, G N ^a   Richards, B E ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; DELTA WING AIRCRAFT; MATHEMATICAL MODELS; REYNOLDS NUMBER; STRUCTURAL ANALYSIS; WALLS (STRUCTURAL PARTITIONS);

DELTA WINGS; GENERALIZED CONJUGATE GRADIENT (GCG) MTHOD; SUPPORT STRUCTURES; WIND-TUNNEL WALLS;

WIND TUNNELS;

EID: 10044239449     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000336     Document Type: Article

References (13)

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3. Engineering Sciences Data Unit, Blockage corrections for bluff bodies in confined flows, 1980, Item 80024, London.
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7. VERHAAGEN, N.G., HOUTMAN, E.M. and VERHELST, J.M. A study of wall effect on the flow over a delta wing, 1996, AIAA-96-2389.
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10. TAYLOR, G., GURSUL, I. and GREENWELL, D. Static hysteresis of vortex breakdown due to support interference, 2001, AIAA 2001-2452.
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12. ERICSSON, L.E. Effect of fuselage geometry on delta-wing vortex breakdown, J Aircr, November-December 1998, 35, (6).
13. ERICSSON, L.E. Further analysis of fuselage effects on delta wing aerodynamics, January 2000, AIAA 2000-0891.