Modeling and aeroelasticity of advanced aircraft wings carrying external stores

American Society of Mechanical Engineers, Aerospace Division (Publication) AD

Volumn 53, Issue , 1997, Pages 185-191

  Gern, Frank H ^a   Librescu, Liviu ^a  

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY CONDITIONS; FUNCTIONS; LAMINATED COMPOSITES; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); VARIATIONAL TECHNIQUES;

FREE BODY MOTIONS; GALERKIN'S METHOD;

WINGS;

EID: 5844379827     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (20)

1. AGARD, 1975, Specialists Meeting on Wing-With-Stores Flutter, AGARD-CP-162, 1975.
2. Flax, A.H., 1961, "Aeroelasticity and Flutter, High Speed Problems of Aircraft and Experimental Methods," Vol. VIII, High Speed Aerodynamics and Jet Propulsion, ed. by H.F. Donavan and H.R. Lawrence, Princeton University Press, Princeton, NJ, 1961, pp. 161-417.
3. Försching, H., 1994, "New Ultra High Capacity Aircraft (UHCA) - Challenges and Problems from an Aeroelastic Point of View", ZFW, J. of Flight Sciences and Aerospace Research, Vol. 18, 1994, pp. 219-231.
4. Goland, M., 1945, "The Flutter of a Uniform Cantilever Wing," Journal of Applied Mechanics, Vol. 12, No. 4, December 1945, pp. A-197-A-208.
5. Hönlinger, H., 1977, "Active Flutter Suppression on an Airplane with Wing Mounted External Stores," AGARD CP 228, April 1977, pp. 3.1-3.15.
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7. Karpouzian, G. and Librescu, L., 1997, "Exact Flutter Solution of Advanced Anisotropic Composite Cantilevered Wing Structures," Proceedings of the 34th SDM Structures, Structural Dynamics and Materials Conference, April 1993, La Jolla, CA, AIAA Paper-93-1536-CR.
8. Karpouzian, G., Librescu, L., 1994 "Comprehensive Model of Anisotropic Composite Aircraft Wings Suitable for Aeroelastic Analyses," J. Aircraft, Vol. 31, No. 3, May-June 1994, pp. 703-712.
9. Librescu, L., 1975, "Elastostatics and Kinematics of Anisotropic and Heterogeneous Shell-Type Structures," Leyden, The Netherlands, Noordhoff International Publishing, 1975.
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11. Librescu, L., Simovich, J., 1988, "General Formulation for the Aeroelastic Divergence of Composite Swept-Forward Wing Structures," J. Aircraft, Vol. 25, No. 4, April 1988, pp. 364-371.
12. Lottati, I., 1987, "Aeroelastic Stability Characteristics of a Composite Swept Wing with Tip Weights for an Unrestrained Vehicle," J. Aircraft, Vol. 24, No. 11, Nov. 1987, pp. 793-802.
13. Lottati, I., 1988, "Aeroelastic Tailoring of a Composite Wing with a Decoupler Pylon as a Wing/Store Flutter Suppressor," J. Aircraft, Vol. 25, No. 3, March 1988, pp. 271-280.
14. Noll, T.E., Huttsell, L.J., Cooley, D.E, 1981, "Wing/Store Flutter Suppression Investigation", J. Aircraft, Vol. 18, No. 11, Nov. 1981, pp. 969-975.
15. Pollock, S.J., Sotomayer, W.A., Huttsell, L.J., Cooley, D.E., 1981, "Evaluation of Methods for Prediction and Prevention of Wing/Store Flutter," AIAA Paper 81-0606, 1981.
16. Reed, W.H., Foughner, J.T., Runyan, H.L., 1980, Decoupler Pylon: A Simple, Effective Wing/Store Flutter Suppressor," J. Aircraft, Vol. 17, No. 3, March 1980, pp. 206-211.
17. Reed, W.H., Cazier, F.W., Foughner, J.T., 1980a, "Passive Control of Wing/Store Flutter," NASA TM81865, 1980.
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19. Runyan, H.L., 1980, "Effect of a Flexibly Mounted Store on the Flutter Speed of a Wing," NASA-CR-159245, April 1980.
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