What was learned from the numerical simulations for the VFE-2

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Fritz, Willy ^a   Cummings, Russell M ^b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLUNT LEADING EDGES; COMPUTATIONAL SIMULATION; DELTA WINGS; EXPERIMENTAL DATA; FLOW EXPERIMENTS; FLOW FEATURES; LEADING EDGE; NUMERICAL SIMULATION; PARTICLE IMAGE VELOCIMETRIES; PRESSURE SENSITIVE PAINTS; PRIMARY VORTEX; SURFACE FLOW; SURFACE PRESSURES; TEST CASE; TRANSITION MODELING; TURBULENCE MODELING;

AEROSPACE ENGINEERING; FLOW VISUALIZATION; VELOCITY MEASUREMENT;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78149427429     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

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12. Fritz, W., "Numerical Simulation of the Peculiar Subsonic Flow- Field about the VFE- 2 Delta-Wing with Rounded Leading-Edge, " AIAA Paper 2008-0393, Jan. 2008.
13. Gürdamar, E., "Influence of Grid Resolution on the Accuracy of High Angle of Attack Delta Wing Simulations, " AIAA Paper 2008-0394, Jan. 2008.
14. Schiavetta, L., Boelens, O.J., Crippa, S., Cummings, R.M., Fritz, W., and Badcock, K.J., "Shock Effects on Delta Wing Vortex Breakdown, " AIAA Paper 2008-0395, Jan. 2008.
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19. Konrath, R., Schröder, A., and Kompenhans, J., "Analysis of PIV Results Obtained for the VFE-2 65 Delta Wing Configuration at Sub- and Transonic Speeds, " AIAA Paper 2006-3003, June 2006.