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Aeroelasticity of Thin-Walled Aircraft Wings

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References

  • Bisplinghoff, R. L., Ashley, H. and Halfman, R. L. (1996) Aeroelasticity, Dover Publications Inc., New York.

    Google Scholar 

  • Cesnik, C. E. S., Hodges, D. H. and Patil, M. J. (1996) “Aeroelastic Analysis of Composite Wings,” AIAA-96-1444-CP.

    Google Scholar 

  • Chattopadhyay, A., Zhang, S. and Jha, R. (1996) “Structural and Aeroelastic Analysis of Composite Wing Box Sections Using Higher-Order Laminate Theory,” AIAA-96-1567-CP.

    Google Scholar 

  • Crawley, E. F. (1994) “Intelligent Structures of Aerospace: A Technology Overview and Assessment,” AIAA Journal, Vol. 31, No. 8, pp. 1689–1699.

    Google Scholar 

  • Diederich, F.W. and Budiansky, C. (1948) “Divergence of Swept Wings,” NACA Technical Note, 1680.

    Google Scholar 

  • Dowell, E. H. (Ed.) (1995) A Modern Course in Aeroelasticity, 3rd Edn., Kluwer Academic Publishers, Boston, MA.

    Google Scholar 

  • Flax, H. H. (1961) “Aeroelasticity and Flutter in High Speed Problems of Aircraft and Experimental Methods,” Vol. VIII High Speed Aerodynamic and Jet Propulsion, eds. Donovan, H. F. and Lawrence, H. R., Princeton University Press, pp. 161–417.

    Google Scholar 

  • Fung, T. C. (1955) An Introduction to the Theory of Aeroelasticity, John Wiley and Sons, New York.

    Google Scholar 

  • Gasbarri, P., Mannini, A. and Barboni, R. (2002) “Dynamic Modeling of Swept Wing with PTFE Method,” Computers and Structures, Vol. 80, pp. 1255–1260.

    Article  Google Scholar 

  • Gern, F. H. and Librescu, L. (1998) “Effects of Externally Mounted stores on Flutter Characteristics of Advanced Swept Cantilevered Aircraft Wings,” Aerospace Science and Technology, Vol. 2, No. 5, pp. 321–333.

    Article  Google Scholar 

  • Gern, F.H. and Librescu, L. (1999a) “Aeroelastic Tailoring of Advanced Aircraft Wings Carrying External Stores,” Atti della Accademia delle Scienze di Torino, Classe di Scienze Fisiche, Mathematiche’e Naturali, Quaderni 1, pp. 201–219 (Issue devoted to Placido Cicala).

    Google Scholar 

  • Gern, F.H. and Librescu, L. (1999b) “Synergistic Interaction of Aeroelastic Tailoring and Boundary Moment Control on Aircraft Wing Flutter,” in Proceedings of the CEAS/AIAA/ICASE /NASA Langley International Forum on Aeroelasticity and Structural Dynamics, June 22–25, Williamsburg, VA, pp. 719–733.

    Google Scholar 

  • Gern, F. H. and Librescu, L. (2000) “Aeroelastic Tailoring of Composite Wings Exhibiting Nonclassical Effects and Carrying External Stores,” Journal of Aircraft, Vol. 37, No. 6, pp. 1097–1004.

    Google Scholar 

  • Gern, F. H. and Librescu, L. (2001) “Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores,” AIAA Journal, Vol. 36, No. 7, pp. 1121–1129.

    Google Scholar 

  • Goland, M. and Luke, Y. (1948) “The Flutter of a Uniform Cantilever Wing with Tip Weights,” Journal of Applied Mechanics, Vol. 15, No. 1, pp. 13–20.

    Google Scholar 

  • Heeg, J. (1991) “Flutter Suppression Via Piezoelectric Actuation,” NASA TM-104120.

    Google Scholar 

  • Hertz, T. J., Shirk, M. H., Ricketts, R. H. and Weisshaar, T. A., (1982) “On the Track of Practical Forward-Swept Wings,” Astronautics and Aeronautics, Vol. 20, January, pp. 40–52.

    Google Scholar 

  • Hollowell, S. J. and Dugundji, J. (1982) “Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite/Epoxy, Cantilevered Plates,” AIAA Paper 82-0722, May.

    Google Scholar 

  • Housner, J. M. and Stein, M. (1974) “Flutter Analysis of Swept-Wing Subsonic Aircraft With Parameter Studies of Composite Wings,” NASA TN-D7539, September.

    Google Scholar 

  • Hwu, C. and Tsai, Z. S. (2002) “Aeroelastic Divergence of Stiffened Composite Multicell Wings Structures,” Journal of Aircraft, Vol. 38, No. 2, pp. 2242–2251.

    Google Scholar 

  • Jha, R. and Chattopadhyay, A. (1997) “Development of a Comprehensive Aeroelastic Analysis Procedure for Composite Wings Using Laplace Domain Methodology,” AIAA 97-1026-CP.

    Google Scholar 

  • Kapania, K. K. and Castel, F. (1990) “A Simple Element for Aeroelastic Analysis of Undamaged and Damaged Wings,” AIAA Journal, Vol. 28, No. 2, pp. 329–337.

    Google Scholar 

  • Karpouzian, G. and Librescu, L. (1994) “A Comprehensive Model of Anisotropic Composite Aircraft Wings and Its Use in Aeroelastic Analyses,” Journal of Aircraft, Vol. 31, No. 3, pp. 702–712.

    Google Scholar 

  • Karpouzian, G. and Librescu, L. (1995) “Exact Flutter Solution of Advanced Composite Swept Wings in Various Flight Speed Regimes,” in Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, New Orleans, LA, April 10–12, AIAA Paper 95-1382.

    Google Scholar 

  • Karpouzian, G. and Librescu, L. (1996) “Non-Classical Effects on Divergence and Flutter of Anisotropic Swept Aircraft Wings,” AIAA Journal, Vol. 34, No. 4, April, pp. 786–794.

    Google Scholar 

  • Kim, D-H. and Lee I. (2001) “Transonic and Supersonic Flutter Characteristics of a Wing-Box Model with Tip Stores,” AIAA-2001-1464.

    Google Scholar 

  • Krone, N. J. Jr. (1975) “Divergence Elimination with Advanced Composites,” AIAA Paper 75-1009, August.

    Google Scholar 

  • Kudva, J. and Lockyear, A. J. (1999) “Exploiting Smart Technologies for Military Aircraft Applications — Perspectives on Development of a Smart Air Vehicle,” in 40th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA/ASME/AHS Adaptive Structures Forum, AIAA Forum on Non-Deterministic Approaches Conference and Exhibit, April 12–15, St. Louis, Missouri, AIAA 99-1511.

    Google Scholar 

  • Lazarus, K. B., Crawley, E. F. and Bohlmann, J. D. (1991) “Static Aeroelastic Control Using Strain Actuated Adaptive Structures,” Journal of Intelligent Material Systems and Structures, Vol. 2, No. 3, July, pp. 386–410.

    Google Scholar 

  • Lee, I. and Miura, H. (1987) “Static Aeroelastic Analysis for Generic Configuration Aircraft,” NASA TM 89423, June, pp. 6–11.

    Google Scholar 

  • Lee, I. and Lee, J. J. (1990) “Vibration Analysis of Composite Plate Wings,” Computers and Structures, Vol. 37, No. 6, pp. 1077–1085.

    Article  Google Scholar 

  • Lee, I., Kim, S. H. and Miura, H. (1994) “Static Aeroelastic Characteristics of a Composite Wing,” Journal of Aircraft, Vol. 31, No. 6, pp. 1413–1416.

    Google Scholar 

  • Lee, U. (1995) “Equivalent Dynamic Beam-Rod Models of Aircraft Wing Structures,” Aeronautical Journal, Vol. 99, December, pp. 450–457.

    Google Scholar 

  • Lehman, L. L. (1982) “A Hybrid State Vector Approach to Aeroelastic Analysis,” AIAA Journal, Vol. 20, No. 10, October, pp. 1442–1449.

    MATH  Google Scholar 

  • Leishman, J. (1988) “Validation of Approximate Indicial Aerodynamic Functions for Two-Dimensional Subsonic Flow,” Journal of Aircraft, Vol. 25, No. 10, pp. 914–922.

    Google Scholar 

  • Leishman, J. (1993) “Indicial Lift Approximations for Two-Dimensional Subsonic Flow as Obtained from Oscillatory Measurements,” Journal of Aircraft, Vol. 30, No. 3, pp. 340–351.

    Google Scholar 

  • Librescu, L. (1975) Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures, Noordhoff International Publishers, Leyden. The Netherlands.

    Google Scholar 

  • Librescu, L. and Khdeir, A. A. (1988) “Aeroelastic Divergence of Swept-Forward Composite Wings Including Warping Restraint Effect,” AIAA Journal, Vol. 26, No. 11, November, pp. 1373–1377.

    Google Scholar 

  • Librescu, L. and Simovich, J. (1988) “General Formulation for the Aeroelastic Divergence of Composite Swept-Forward Wing Structures,” Journal of Aircraft, Vol. 25, No. 4, April, pp. 364–371.

    Google Scholar 

  • Librescu, L. and Song, O. (1990) “Static Aeroelastic Tailoring of Composite Aircraft Wings Modelled as Thin-Walled Beam Structures,” in Achievements in Composites in Japan and the United States, Fifth Japan-U.S. Conference on Composite Materials, A. Kobayashi (Ed.), Kokon Shoin Co., Tokyo, pp. 141–149.

    Google Scholar 

  • Librescu, L. and Song, O. (1992) “On the Static Aeroelastic Tailoring of Composite Aircraft Swept Wings Modelled as Thin-Walled Beam Structures,” Composites Engineering, Vol. 2, Nos. 5–7 (Special Issue: Use of Composites in Rotorcraft and Smart Structures), pp. 497–512.

    Google Scholar 

  • Librescu, L. and Thangjitham, S. (1991) “Analytical Studies on Static Aeroelastic Behavior of Forward Swept Composite Wing Structures,” Journal of Aircraft, Vol. 28, No. 2, February, pp. 151–157.

    Google Scholar 

  • Librescu, L., Meirovitch, L. and Song, O. (1996a) “Integrated Structural Tailoring and Control Using Adaptive Materials for Advanced Aircraft Wings,” Journal of Aircraft, Vol. 30, No. 1, January-February, pp. 203–213.

    Google Scholar 

  • Librescu, L., Meirovitch, L. and Song, O. (1996b) “Refined Structural Modeling for Enhancing Vibrations and Aeroelastic Characteristics of Composite Aircraft Wings,” La Recherche Aérospatiale, No. 1, pp. 23–35.

    Google Scholar 

  • Livne, E., Schmidt, L. A. and Friedmann, P. P. (1990) “Towards Integrated Multidisciplinary Synthesis of Actively Controlled Fiber Composite Wings,” Journal of Aircraft, Vol. 27, No. 12, pp. 979–992.

    Google Scholar 

  • Livne, E., Schmidt, L.A. and Friedmann, P. P. (1993) “Integrated Structure/Control/Aerodynamic Synthesis of Actively Controlled Composite Wings,” Journal of Aircraft, Vol. 30, No. 3, May-June, pp. 387–394.

    Google Scholar 

  • Lottati, I. (1985) “Flutter and Divergence Aeroelastic Characteristics for Composite Forward Swept Cantilevered Wing,” Journal of Aircraft, Vol. 22, No. 11, pp. 1001–1007.

    Google Scholar 

  • Lottati, I. (1987) “Aeroelastic Stability Characteristics of a Composite Swept Wings with Tip Weights For an Unrestrained Vehicle,” Journal of Aircraft, Vol. 24, No. 11, pp. 793–812.

    Google Scholar 

  • Marzocca, P., Librescu, L. and Chiocchia, G. (2001) “Aeroelastic Response of 2-D Lifting Surfaces to Gust and Arbitrary Explosive Loading Signatures,” International Journal of Impact Engineering, Vol. 25, No. 1, pp. 41–65.

    Article  Google Scholar 

  • Marzocca, P., Librescu, L. and Chiocchia, G. (2002) “Aeroelasticity of Two-Dimensional Lifting Surfaces via Indicial Function Approach,” The Aeronautical Journal, Vol. 39, No. 1057, pp. 147–153.

    Google Scholar 

  • Marzocca, P., Librescu, L. and Silva, W. A. (2002) “Unified Approach of Aeroelastic Response and Flutter of Swept Aircraft Wings in an Incompressible Flow,” AIAA Journal, Vol. 40, No. 5, pp. 801–812.

    Google Scholar 

  • Marzocca, P., Librescu, L. and Chiocchia, G. (2002) “Aeroelastic Response of a 2-D Airfoil in a Compressible Flow Field and Exposed to Blast Loading,” Aerospace Science and Technology, Vol. 6, No. 4, pp. 259–272.

    Article  Google Scholar 

  • Marzocca, P., Librescu, L. and Chiocchia, C. (2002) “Unsteady Aerodynamics in Various Flight Speed Regimes for Flutter/Dynamic Response Analyses,” in Proceeding of the 18th AIAA Applied Aerodynamic Conference, Denver, CO, August 14–17, AIAA-2000-4229.

    Google Scholar 

  • Marzocca, P., Librescu, L., Kim, D. and Lee, I. (2003) “Linear/Nonlinear Unsteady Aerodynamic Modeling of 2-D Lifting Surfaces Via a Combined CDF/Analytical Approach,” AIAA-2003-1925, 7–10 April, Norfolk, VA.

    Google Scholar 

  • McGowan, A-M. R., Heeg, J. and Lake, R. C. (1996) “Results of Wing-Tunnel Testing from the Piezoelectric Aeroelastic Response Tailoring Investigation,” AIAA-96-1511-CP.

    Google Scholar 

  • Nam, C. and Kim, Y. (1995) “Optimal Design of Composite Lifting Surface for Flutter Suppressions with Piezoelectric Actuators,” AIAA Journal, Vol. 33, No. 10, October.

    Google Scholar 

  • Nam, C., Chattopadhyay, A. and Kim, Y. (2001) “Aeroelastic Control of Smart Composite Plate with Delaminations,” Journal of Intelligent Material Systems and Structures, Vol. 11, pp. 868–876.

    Google Scholar 

  • Niblett, L. T. (1980) “Divergence and Flutter of Swept-Forward Wings with Cross Flexibilities,” RAE-TR-80047, April.

    Google Scholar 

  • Oyibo, G. A. and Berman, J. H. (1985) “Anisotropic Wing Aeroelastic Theories with Warping Effects,” Second International Symposium on Aeroelasticity and Structural Dynamics, Aachen, FRG, April.

    Google Scholar 

  • Oyibo, G. A. (1989) “Some Implications of Warping Restraint on the Behavior of Composite Anisotropic Beams,” Journal of Aircraft, February, Vol. 26, No. 2, pp. 187–189.

    Google Scholar 

  • Patil, M. J., Hodges, D. H. and Cesnik, C. E. S. (2000) “Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow,” Journal of Aircraft, Vol. 37, No. 5, pp. 753–760.

    Google Scholar 

  • Petre, A., Stanescu, C. and Librescu, L. (1961) “Aeroelastic Divergence of Multicell Wings Taking Their Fixing Restraints into Account,” Revue de Mecanique Appliquee, Vol. 19, No. 6, pp. 689–698.

    Google Scholar 

  • Qin, Z. (2001) Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams, Ph.D. Thesis, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, October, Department of Engineering Science and Mechanics.

    Google Scholar 

  • Qin, Z., Marzocca, P. and Librescu, L. (2002) “Aeroelastic Instability and Response of Advanced Aircraft Wings at Subsonic Flight Speeds,” Aerospace Science and Technology, Vol. 6, No. 3, pp. 195–208.

    Article  Google Scholar 

  • Qin, Z. and Librescu, L. (2003a) “Aeroelastic Instability of Aircraft Wings Modeled as Anisotropic Composite Thin-Walled Beams in the Compressible Flow,” Journal of Fluid and Structures, Vol. 19, No. 1, pp. 43–61.

    Google Scholar 

  • Qin, Z. and Librescu, L. (2003b) “Dynamic Aeroelastic Response of Aircraft Wings Modeled as Anisotropic Thin-Walled Beams,” Journal of Aircraft, Vol. 40, No. 3, pp. 532–543.

    Google Scholar 

  • Qin, Z., Librescu, L. and Marzocca, P. (2003) “Aeroelasticity of Composite Aerovehicle Wings in Supersonic Flows,” Journal of Spacecraft and Rockets, Vol. 40, No. 2, pp. 162–173.

    Google Scholar 

  • Rodden, W. P. and Stahl, B. (1969) “A Strip Method for Prediction of Damping in Subsonic Wind Tunnel and Flight Flutter Tests,” Journal of Aircraft, Vol. 6, No. 1, pp. 9–17.

    Google Scholar 

  • Sherrer, V. C., Hertz, T. J. and Shirk, M. H. (1981) “Wing Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept Wings,” Journal of Aircraft, Vol. 19, Nov., pp. 976–903.

    Google Scholar 

  • Shirk, M. H., Hertz, t. J. and Weisshaar, T. A. (1986) “Aeroelastic Tailoring — Theory, Practice and Promise,” Journal of Aircraft, Vol. 23, No. 1, January, pp. 6–18.

    Google Scholar 

  • Singh, R. and Baeder, J. D. (1997) “Direct Calculation of Three-Dimensional Indicial Lift Response Using Computational Fluid Dynamics,” Journal of Aircraft, Vol. 34, No. 4, pp. 465–471.

    Google Scholar 

  • Song, O., Librescu, L. and Rogers, C. A. (1992) “Application of Adaptive Technology to Static Aeroelastic Control of Wing Structures,” AIAA Journal, Vol. 30, No. 12, pp. 2882–2889.

    Google Scholar 

  • von Kármán, T. and Sears, W. R. (1938) “Airfoil Theory for Non-Uniform Motion,” Journal of the Aeronautical Sciences, Vol. 5, No. 10, pp. 379–390.

    Google Scholar 

  • Weisshaar, T. A. (1978) “Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Swept Forward Wing Structures,” AFFDL-TR-78-116, September.

    Google Scholar 

  • Weisshaar, T. A. (1979) “Forward Swept Wing. Static Aeroelasticity,” AFFDL-TR-3087, June.

    Google Scholar 

  • Weisshaar, T. A. (1980) “Divergence of Forward Swept Composite Wings,” Journal of Aircraft, Vol. 17, June, pp. 442–448.

    Google Scholar 

  • Weisshaar, T. A. (1981) “Aeroelastic Tailoring of Forward Swept Composite Wings,” Journal of Aircraft, Vol. 18, pp. 669–676.

    Google Scholar 

  • Weisshaar, T. A. (1987) “Aeroelastic Tailoring-Creative Use of Unusual Materials,” in AIAA/ASME/ASCE/AHS 28th Structures, Structural Dynamics and Materials Conference, Monterey, CA, April 9–10, AIAA Paper 87-0976.

    Google Scholar 

  • Weisshaar, T. A. and Ehlers, S. M. (1992) “Adaptive Aeroelastic Composite Wings–Control and Optimization Issues,” Composites Engineering, Vol. 2, Nos. 5–7, pp. 457–476.

    Google Scholar 

  • Yates, E. C., Jr. (1958) “Calculation of Flutter Characteristics for Finite-Span Swept or Unswept Wings at Subsonic and Supersonic Speeds by a Modified Strip Analysis,”NACARML57L10.

    Google Scholar 

  • Yamane, T. and Friedmannn, P. P. (1993) “Aeroelatic Tailoring for Preliminary Design of Advanced Propellers with Composite Blades,” Journal of Aircraft, Vol. 30, No. 1, pp. 119–126.

    Google Scholar 

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(2006). Aeroelasticity of Thin-Walled Aircraft Wings. In: Thin-Walled Composite Beams. Solid Mechanics and Its Applications, vol 131. Springer, Dordrecht. https://doi.org/10.1007/1-4020-4203-5_12

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