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Volumn 37, Issue 1, 2000, Pages 37-44

Experiments on a 60-degree delta wing with rounded leading-edge vortex flaps

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WING AIRCRAFT; DRAG; FORCE MEASUREMENT; LIFT; PRESSURE MEASUREMENT; REYNOLDS NUMBER; WIND TUNNELS;

EID: 0033882814     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2559     Document Type: Article
Times cited : (15)

References (18)
  • 1
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  • 2
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    • Effectiveness of Leading-Edge Vortex Flaps on 60- and 75-Degree Delta Wings
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  • 3
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    • An Investigation of the Tabbed Vortex Flap
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  • 4
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    • Subsonic Wind-Tunnel Measurements of a Slender Wing-Body Configuration Employing a Vortex Flap
    • July
    • Frink, N. T., "Subsonic Wind-Tunnel Measurements of a Slender Wing-Body Configuration Employing a Vortex Flap," NASA TM-89101, July 1987.
    • (1987) NASA TM-89101
    • Frink, N.T.1
  • 5
    • 0028393127 scopus 로고
    • Experimental Studies of Vortex Flaps and Vortex Plates
    • Rinoie, K., and Stollery, J. L., "Experimental Studies of Vortex Flaps and Vortex Plates," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 322-329.
    • (1994) Journal of Aircraft , vol.31 , Issue.2 , pp. 322-329
    • Rinoie, K.1    Stollery, J.L.2
  • 6
    • 0028464287 scopus 로고
    • Experimental Investigation of Vortex Flaps on Thick Delta Wings
    • Levin, D., and Seigner, A., "Experimental Investigation of Vortex Flaps on Thick Delta Wings," Journal of Aircraft, Vol. 31, No. 4, 1994, pp. 988-991.
    • (1994) Journal of Aircraft , vol.31 , Issue.4 , pp. 988-991
    • Levin, D.1    Seigner, A.2
  • 7
    • 0029276904 scopus 로고
    • Aerodynamic Characteristics of Vortex Flaps on a Double-Delta Planform
    • Traub, L. W., "Aerodynamic Characteristics of Vortex Flaps on a Double-Delta Planform," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 449, 450.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 449
    • Traub, L.W.1
  • 8
    • 0030285939 scopus 로고    scopus 로고
    • Effect of Leading-Edge Flaps on Vortices and Vortex Breakdown
    • Deng, Q., and Gursul, I., "Effect of Leading-Edge Flaps on Vortices and Vortex Breakdown," Journal of Aircraft, Vol. 33, No. 6, 1996, pp. 1079-1086.
    • (1996) Journal of Aircraft , vol.33 , Issue.6 , pp. 1079-1086
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  • 9
    • 0031223090 scopus 로고    scopus 로고
    • Experimental Studies of a 70-Degree Delta Wing with Vortex Flaps
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    • Rinoie, K.1    Fujita, T.2    Iwasaki, A.3    Fujieda, H.4
  • 11
    • 6744256827 scopus 로고
    • Low-Speed Experimental Determination of the Effects of Leading-Edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing
    • July
    • Fletcher, H. S., "Low-Speed Experimental Determination of the Effects of Leading-Edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing," NACA TN-4341, July 1958.
    • (1958) NACA TN-4341
    • Fletcher, H.S.1
  • 12
    • 6744238813 scopus 로고
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    • Dec.
    • Henderson, W. P., "Effects of Wing Leading-Edge Radius and Reynolds Number on Longitudinal Aerodynamic Characteristics of Highly Swept Wing-Body Configurations at Subsonic Speeds," NACA TN D-8361, Dec. 1976.
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  • 13
    • 0012314391 scopus 로고    scopus 로고
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    • Feb.
    • Chu, J., and Luckring, M., "Experimental Surface Pressure Data Obtained on 65° Delta Wing Across Reynolds Number and Mach Number Ranges," NASA TM 4645, Feb. 1996.
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  • 14
    • 6744225390 scopus 로고
    • The Performance of 60° Delta Wings: The Effects of Leading Edge Radius and Vortex Flaps
    • Cranfield Inst. of Technology, Bedford, England, U.K., March
    • Hu, B. K., and Stollery, J. L., "The Performance of 60° Delta Wings: The Effects of Leading Edge Radius and Vortex Flaps," College of Aeronautics Rept. No.9004, Cranfield Inst. of Technology, Bedford, England, U.K., March 1990.
    • (1990) College of Aeronautics Rept. No.9004
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  • 15
    • 6744223865 scopus 로고    scopus 로고
    • Low Speed Aerodynamic Characteristics of 60° Rounded Leading-Edge Delta Wing with Vortex Flaps: Part 1. 457.2mm Span Delta Wing
    • Cranfield Univ., Bedford, England, U.K., Dec.
    • Rinoie, K., "Low Speed Aerodynamic Characteristics of 60° Rounded Leading-Edge Delta Wing with Vortex Flaps: Part 1. 457.2mm Span Delta Wing," College of Aeronautics Rept. 9611, Cranfield Univ., Bedford, England, U.K., Dec. 1996.
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    • Rinoie, K.1
  • 16
    • 0015021235 scopus 로고
    • Vortex Breakdown on Slender Sharp-Edged Wings
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  • 17
    • 0030196820 scopus 로고    scopus 로고
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    • Traub, L.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.