SCOPUS 정보 검색 플랫폼

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

Experimental and CFD contribution to delta wing vortical flow understanding

(3) Le Roy, Jean François a Rodriguez, Ovide a Kurun, Suleyman b

a ONERA (France)

b SCIENTIFIC AND TECHNOLOGICAL RESEARCH COUNCIL OF TURKEY (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

2-D PIV; COMPUTATIONAL RESULTS; COMPUTATIONAL WORK; DATA SETS; DELTA WINGS; EXPERIMENTAL DATA; LEADING EDGE; LOW MACH NUMBERS; MAIN CHARACTERISTICS; MOMENT MEASUREMENTS; PRESSURE SURFACE; SECONDARY VORTEX; SEPARATED FLOWS; STEREOSCOPIC PIV; UPPER SURFACE; VORTEX BREAKDOWN LOCATION; VORTICAL FLOWS; W MODEL; WIND TUNNEL EXPERIMENT;

AERODYNAMICS; AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; DELTA WING AIRCRAFT; FEATURE EXTRACTION; MACH NUMBER; REYNOLDS NUMBER; TURBULENCE MODELS; TWO DIMENSIONAL; VORTEX FLOW; WIND TUNNELS;

DATA FLOW ANALYSIS;

EID: 78149432596 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper

Times cited : (18)

References (9)

1
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- Paper No. 15, January, AGARD CP-247
- Hummel, D., "On the Vortex Formation Over a Slender Wing at Large Incidence" AGARD CP-247, Paper No.15, January 1979.
- (1979) On the Vortex Formation Over a Slender Wing at Large Incidence
- Hummel, D.¹

2
- 0003587703
- AIAA Paper 93-0050, Jan.
- Rockwell, D., "Three Dimensional Flow Structure on Delta Wings at High Angle-of-Attack: Experimental Concepts and Issues, " AIAA Paper 93-0050, Jan.1993.
- (1993) Three Dimensional Flow Structure on Delta Wings at High Angle-of-Attack: Experimental Concepts and Issues
- Rockwell, D.¹

3
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- Aspects of vortex breakdown
- Delery, J., "Aspects of Vortex Breakdown, " Progress in Aerospace Sciences, Vol.30, N°1, 1994, pp.1, 59.
- (1994) Progress in Aerospace Sciences , vol.30 , Issue.1 , pp. 1-59
- Delery, J.¹

4
- 33845785586
- AIAA Paper 95-0585, Jan.
- Visbal, M. R., "Computational and Physical Aspects of Vortex Breakdown on Delta Wings, " AIAA Paper 95-0585, Jan.1995.
- (1995) Computational and Physical Aspects of Vortex Breakdown on Delta Wings
- Visbal, M.R.¹

5
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- Experimental surface pressure data obtained on 65° delta wing across reynolds number and mach number ranges
- Langley Research Center. Hampton, Virginia. February
- Chu, J. and Luckring, J. M., "Experimental Surface Pressure Data Obtained on 65° Delta Wing Across Reynolds number and Mach Number Ranges". NASA Technical Memorandum 4645. Langley Research Center. Hampton, Virginia. February 1996.
- (1996) NASA Technical Memorandum 4645
- Chu, J.¹ Luckring, J.M.²

6
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- Reynolds number, compressibility, and leading edge bluntness effects on delta wing aerodynamic
- th International Congress of the Aerodynamic Sciences.
- th International Congress of the Aerodynamic Sciences
- Luckring, J.M.¹

7
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- Elsa: An efficient object-oriented solution to CFD complexity
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- th AIAA Aerospace Science Meeting and Exhibit. Reno (USA), January 14-17, 2002.
- (2002) th AIAA Aerospace Science Meeting and Exhibit
- Cambier, L.¹ Gazaix, M.²

8
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- EADS-M Technical note
- W. Fritz: "VFE-2 Delta Wing Structured Grids". EADS-M Technical note.
- VFE-2 Delta Wing Structured Grids
- Fritz, W.¹

9
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- Analysis of PSP results obtained for the VFE-2 65° delta wing configuration at sub- and transonic speeds
- Reno (USA), January 9-12
- th AIAA Aerospace Science Meeting and Exhibit. Reno (USA), January 9-12, 2006.
- (2006) th AIAA Aerospace Science Meeting and Exhibit
- Konrath, R.¹ Klein, C.² Engler, R.³ Otter, D.⁴

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