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Volumn 7, Issue , 2003, Pages 4937-4947

Effect of compressive force on flutter speed of a strut-braced wing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; BUCKLING; COMPRESSIVE STRESS; DEFORMATION; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); SPEED; STIFFNESS; STRUTS;

EID: 0041475918     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (34)
  • 2
    • 0005887991 scopus 로고
    • The effect on block fuel consumption of a strutted vs. cantilever wing for a short haul transport including strut aeroelastic considerations
    • AIAA-78-1454-CP, Los Angeles, California, Aug. 21-23
    • Park, H. P., "The Effect on Block Fuel Consumption of a Strutted vs. Cantilever Wing for a Short Haul Transport Including Strut Aeroelastic Considerations," AIAA-78-1454-CP, Los Angeles, California, Aug. 21-23, 1978.
    • (1978)
    • Park, H.P.1
  • 3
    • 0005814696 scopus 로고    scopus 로고
    • Wing planform geometry effects on large subsonic military transport airplanes
    • Boeng Commercial Airplane Company, AFFDL-TR-78-16, February
    • Kulfan, R.M., and Vachal, J.D., "Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes," Boeng Commercial Airplane Company, AFFDL-TR-78-16, February 1978.
    • Kulfan, R.M.1    Vachal, J.D.2
  • 4
    • 0035083478 scopus 로고    scopus 로고
    • Structural wing sizing for multidisciplinary design optimization of a strut-braced wing
    • Gern, F.H., Naghshineh-Pour, A., Sulaeman, E., Kapania, R.K., and Haftka, R.T., "Structural Wing Sizing for Multidisciplinary Design Optimization of a Strut-Braced Wing," Journal of Aircraft, Vol. 38, No. 1, 2001.
    • (2001) Journal of Aircraft , vol.38 , Issue.1
    • Gern, F.H.1    Naghshineh-Pour, A.2    Sulaeman, E.3    Kapania, R.K.4    Haftka, R.T.5
  • 5
    • 0005887391 scopus 로고    scopus 로고
    • Structural optimization and design of a strut-braced wing aircraft
    • MS Thesis, Virginia Tech, November
    • Naghshineh-Pour, A.H., "Structural Optimization and Design of a Strut-Braced Wing Aircraft," MS Thesis, Virginia Tech, November 1998.
    • (1998)
    • Naghshineh-Pour, A.H.1
  • 6
    • 0035517181 scopus 로고    scopus 로고
    • Multidisciplinary design optimization of a transonic commercial transport with a surf-braced wing
    • Gern, F.H., Ko, A., Sulaeman, E., Cundlach, J.F., Kapania, R.K., and Haftka, R.T., "Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Surf-Braced Wing," Journal of Aircraft, Vol. 38, No. 6, 2001, pp. 1006-1014.
    • (2001) Journal of Aircraft , vol.38 , Issue.6 , pp. 1006-1014
    • Gern, F.H.1    Ko, A.2    Sulaeman, E.3    Cundlach, J.F.4    Kapania, R.K.5    Haftka, R.T.6
  • 9
    • 0005898307 scopus 로고
    • Izbrannye trudy: Mekanika
    • Moscow, Nauca
    • Keldysh, M.V., Izbrannye trudy: Mekanika, Moscow, Nauca, 1985, pp. 304 - 341.
    • (1985) , pp. 304-341
    • Keldysh, M.V.1
  • 10
    • 0005883559 scopus 로고    scopus 로고
    • The keldysh problem on aeroelastic stability of a strut-braced wing
    • (Translated from original Russian text in Doklady Akademii Nauk, Vol. 350, No.4, 1996)
    • Mailybaev, A.A., and Seiranyan, A.P. "The Keldysh Problem on Aeroelastic Stability of a Strut-braced Wing," Physics-Doklady, Vol. 41, No. 10, 1996, pp. 484-487 (Translated from original Russian text in Doklady Akademii Nauk, Vol. 350, No.4, 1996).
    • (1996) Physics-Doklady , vol.41 , Issue.10 , pp. 484-487
    • Mailybaev, A.A.1    Seiranyan, A.P.2
  • 13
    • 0005849995 scopus 로고    scopus 로고
    • Aeroelastic stability analysis with a geometric stiffness effect of a strut-braced wing
    • PhD. Dissertation, Virginia Tech., November
    • Sulaeman, E. "Aeroelastic Stability Analysis with a Geometric Stiffness Effect of a Strut-Braced Wing," PhD. Dissertation, Virginia Tech., November 2001.
    • (2001)
    • Sulaeman, E.1
  • 14
    • 0041788184 scopus 로고    scopus 로고
    • ZONA Technology,. Inc.; ZONA 01-24-4, Scottsdale, AZ, February
    • ZONA Technology,. Inc., ZAERO Theoretical Manual, Version 5.0, ZONA 01-24-4, Scottsdale, AZ, February 2001.
    • (2001) ZAERO Theoretical Manual, Version 5.0
  • 16
    • 0041287644 scopus 로고
    • A vortex lattice method for the mean camber shapes of trimmed non-coplanar planforms with minimum vortex drag
    • NASA TN D-8090, June
    • Lamar, J.E., "A Vortex Lattice Method for the Mean Camber Shapes of Trimmed Non-Coplanar Planforms with Minimum Vortex Drag," NASA TN D-8090, June 1976.
    • (1976)
    • Lamar, J.E.1
  • 18
    • 0020102987 scopus 로고
    • A new subsonic method for lifting surfaces in subsonic flow
    • March
    • Ueda, T., and Dowell, E.H., "A New Subsonic Method for Lifting Surfaces in Subsonic Flow," AIAA Journal, Vol. 20, No. 3, March 1982, pp. 348-355.
    • (1982) AIAA Journal , vol.20 , Issue.3 , pp. 348-355
    • Ueda, T.1    Dowell, E.H.2
  • 19
    • 85002529705 scopus 로고    scopus 로고
    • A new subsonic method for lifting surfaces in subsonic flow
    • Rodden, W.P., Vol. 22, No. 1, p. 160.
    • AIAA Journal , vol.22 , Issue.1 , pp. 160
    • Rodden, W.P.1
  • 20
    • 0042790382 scopus 로고    scopus 로고
    • A new subsonic method for lifting surfaces in subsonic flow
    • Ueda, T. and Dowell, E.H., Vol. 22, No.4, p.575.
    • AIAA Journal , vol.22 , Issue.4 , pp. 575
    • Ueda, T.1    Dowell, E.H.2
  • 21
    • 0022413459 scopus 로고
    • Nonplanar, subsonic, three-dimensional oscillatory piecewise continuous kernel function method
    • Dec
    • Lottati, I., and Nissim, E., "Nonplanar, Subsonic, Three-Dimensional Oscillatory Piecewise Continuous Kernel Function Method," Journal of Aircraft, Vol. 22, No. 12, Dec 1985, pp. 1043 - 1048.
    • (1985) Journal of Aircraft , vol.22 , Issue.12 , pp. 1043-1048
    • Lottati, I.1    Nissim, E.2
  • 24
    • 0005808878 scopus 로고    scopus 로고
    • Structural and aerodynamic investigation of a strut-braced wing transport aircraft
    • Lockheed Martin Aeronautical Systems Phase 2 Final Report, Dec. 8
    • Anon., "Structural and Aerodynamic Investigation of a Strut-Braced Wing Transport Aircraft", Lockheed Martin Aeronautical Systems Phase 2 Final Report, Dec. 8, 1999.
    • (1999)
    • Anon1
  • 25
    • 84872464957 scopus 로고    scopus 로고
    • Federal Aviation Administration, Department of Transportation, Part 25, Last Updated Date: Dec 1
    • Anon., Airworthiness Standards: Transport Category Airplanes, Federal Aviation Administration, Department of Transportation, Part 25, Last Updated Date: Dec 1, 2001.
    • (2001) Airworthiness Standards: Transport Category Airplanes
    • Anon1
  • 26
    • 85003407026 scopus 로고
    • Kernel function for nonplanar oscillating surfaces in a subsonic flow
    • May
    • Landahl, M.T., "Kernel Function for Nonplanar Oscillating Surfaces in a Subsonic Flow," AIAA Journal, Vol. 4, No. 4, May 1967, pp. 1045-1046.
    • (1967) AIAA Journal , vol.4 , Issue.4 , pp. 1045-1046
    • Landahl, M.T.1
  • 27
    • 0015255754 scopus 로고
    • Refinement of the nonplanar aspects of the subsonic doublet lattice lifting surface method
    • Jan
    • Rodden, W.P., Giesing, J.P., and Kalman, T.P., "Refinement of the Nonplanar Aspects of the Subsonic Doublet Lattice Lifting Surface Method," Journal of Aircraft, Vol. 9, Jan 1972, pp. 69-73.
    • (1972) Journal of Aircraft , vol.9 , pp. 69-73
    • Rodden, W.P.1    Giesing, J.P.2    Kalman, T.P.3
  • 28
    • 0026223208 scopus 로고
    • Hybrid doublet lattice/doublet point method for lifting surfaces in subsonic flow
    • Sept.
    • Eversman, W., and Pitt, D.M., "Hybrid Doublet Lattice/Doublet Point Method for Lifting Surfaces in Subsonic Flow," Journal of Aircraft, Vol. 28, No. 9, Sept. 1991, pp. 572-578.
    • (1991) Journal of Aircraft , vol.28 , Issue.9 , pp. 572-578
    • Eversman, W.1    Pitt, D.M.2
  • 29
    • 0042289273 scopus 로고
    • Asymptotic expansion of the kernel function in subsonic unsteady lifting surface theory
    • Ueda, T., "Asymptotic Expansion of the Kernel Function in Subsonic Unsteady Lifting Surface Theory," Journal of the Japan Society for Aeronautical Space Sciences, Vol 20, No. 326, 1981, pp. 169-174.
    • (1981) Journal of the Japan Society for Aeronautical Space Sciences , vol.20 , Issue.326 , pp. 169-174
    • Ueda, T.1
  • 30
    • 85003292693 scopus 로고
    • Expansion series of integral functions in unsteady aerodynamics
    • April
    • Ueda, T., "Expansion Series of Integral Functions in Unsteady Aerodynamics," Journal of Aircraft, Vol. 19, No. 7, April 1982, pp. 345-347.
    • (1982) Journal of Aircraft , vol.19 , Issue.7 , pp. 345-347
    • Ueda, T.1
  • 31
    • 0023348360 scopus 로고
    • Lifting surface calculations in the laplace domain with application to root loci
    • May
    • Ueda, T., "Lifting Surface Calculations in the Laplace Domain with Application to Root Loci," AIAA Journal, Vol 25, No. 5, May 1987, pp. 698-704.
    • (1987) AIAA Journal , vol.25 , Issue.5 , pp. 698-704
    • Ueda, T.1
  • 32
    • 0032205740 scopus 로고    scopus 로고
    • Arbitrary accuracy integration scheme for the subsonic doublet lattice method
    • Van Zyl, L.H., "Arbitrary Accuracy Integration scheme for the Subsonic Doublet Lattice Method," Journal of Aircraft, Vol. 35, No. 6, pp. 975-977.
    • Journal of Aircraft , vol.35 , Issue.6 , pp. 975-977
    • Van Zyl, L.H.1
  • 33
    • 0032205199 scopus 로고    scopus 로고
    • Convergence of the subsonic doublet lattice method
    • Van Zyl, L.H., "Convergence of the Subsonic Doublet Lattice Method," Journal of Aircraft, Vol. 35, No. 6, pp. 977-979.
    • Journal of Aircraft , vol.35 , Issue.6 , pp. 977-979
    • Van Zyl, L.H.1
  • 34
    • 0029507960 scopus 로고
    • Alternative solution of the kernel function in subsonic unsteady lifting surface theory
    • Epstein, R.J., and Bliss, D.B., "Alternative Solution of the Kernel Function in Subsonic Unsteady Lifting Surface Theory," AIAA Journal, Vo. 33, No. 11, 1995, pp. 2228-2230.
    • (1995) AIAA Journal , vol.33 , Issue.11 , pp. 2228-2230
    • Epstein, R.J.1    Bliss, D.B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.