Volume 19, Issue 4 (2019)                   Modares Mechanical Engineering 2019, 19(4): 927-935 | Back to browse issues page

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Shams S, Keshtgar M, Mansouri M. Aeroelastic Analysis of a Double-Sweep Wing with the Metal/Composite Sections. Modares Mechanical Engineering. 2019; 19 (4) :927-935
URL: http://mme.modares.ac.ir/article-15-17603-en.html
1- Aerospace Engineering Department, New Sciences & TechnologiesFaculty, University of Tehran, Tehran, Iran , shahrokh.shams@ut.ac.ir
2- Aerospace Engineering Department, Aerospace Engineering Faculty, K.N. Toosi University, Tehran, Iran
3- Aerospace Engineering Department, New Sciences & TechnologiesFaculty, University of Tehran, Tehran, Iran
Full-Text [PDF 749 kb]   (641 Downloads)    
Article Type: Original Research | Subject: Aerospace Structures
Received: 2018/11/6 | Accepted: 2018/12/1 | Published: 2019/04/6

1. Lottati I. Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing. Journal of Aircraft. 1985;22(11):1001-1007. [Link] [DOI:10.2514/3.45238]
2. Weisshaar TA. Aeroelastic tailoring-creative use of unusual materials. 28th Structures, Structural Dynamics and Materials Conference, 6-8 April, 1987, Monterey, California, U.S.A. Reston: AIAA; 1987. [Link]
3. Lazarus KB, Crawley EF, Bohlmann JD. Static aeroelastic control using strain actuated adaptive structures. Journal of Intelligent Material Systems and Structures. 1991;2(3):386-410. [Link] [DOI:10.1177/1045389X9100200307]
4. Ehlers SM, Weisshaar TA. Static aeroelastic behaviour of an adaptive laminated piezoelectric composite wing. 31st Structures, Structural Dynamics and Materials Conference, 2-4 April, 1990, Long Beach, California, U.S.A. Reston: AIAA; 1990. [Link]
5. Pai PF, Nayfeh AH. Non-linear non-planar oscillations of a cantilever beam under lateral base excitations. International Journal of Non Linear Mechanics. 1990;25(5):455-474. [Link] [DOI:10.1016/0020-7462(90)90012-X]
6. Anderson TJ, Nayfeh AH, Balachandran B. Experimental verification of the importance of the nonlinear curvature in the response of a cantilever beam. Journal of Vibration and Acoustics. 1996;118(1):21-27. [Link] [DOI:10.1115/1.2889630]
7. Malatkar P, Nayfeh AH. A parametric identification technique for single-degree-of-freedom weakly nonlinear systems with cubic nonlinearities. Journal of Vibration and Control. 2003;9(3-4):317-336. [Link]
8. Weisshaar TA, Foist BL. Vibration tailoring of advanced composite lifting surfaces. Journal of Aircraft. 1985;22(2):141-147. [Link] [DOI:10.2514/3.45098]
9. Bauchau OA, Hong CH. Nonlinear composite beam theory. Journal of Applied Mechanics. 1988;55(1):156-163. [Link] [DOI:10.1115/1.3173622]
10. Pai PF, Nayfe AH. Three dimensional nonlinear vibration of composite beam-I. Equation of motion. Nonlinear Dynamics. 1990;1(6):477-502. [Link] [DOI:10.1007/BF01856950]
11. Haddadpour H, Kouchakzadeh MA, Shadmehri F. Aeroelastic instability of aircraft composite wings in an incompressible flow. Composite Structures. 2008;83(1):93-99. [Link] [DOI:10.1016/j.compstruct.2007.04.012]
12. Jacobsen LS. Natural frequencies of uniform cantilever beams of symmetrical cross- section. Journal of Applied Mechanics, A-1. 1938;5. [Link]
13. Amoozgar MR, Irani S, Vio GA. Aeroelastic instability of a composite wing with a powered-engine. Journal of Fluids and Structures. 2013;36:70-82. [Link] [DOI:10.1016/j.jfluidstructs.2012.10.007]
14. Shams Sh. Investigating the aeroelastic behavior of flexible composite wings with high aspect ratio with nonlinear geometric behavior in incompressible flow [Dissertation]. Tehran: Amirkabir University of Technology; 2008. [persian] [Link]
15. Shams Sh, Sadr Lahidjani MH, Haddadpour H. Nonlinear aeroelastic response of slender wings based on Wagner function. Thin Walled Structures. 2008;46(11):1192-1203. [Link] [DOI:10.1016/j.tws.2008.03.001]
16. Shams Sh, Sadr Lahidjani MH, Haddadpour H. An efficient method for nonlinear aeroelasticy of slender wings. Nonlinear Dynamics. 2012;67(1):659-681. [Link] [DOI:10.1007/s11071-011-0018-2]
17. Patil MJ, Hodges DH, Cesnik CES. Limit-cycle oscillations in high-aspect-ratio wings. Journal of Fluids and Structures. 2001;15(1):107-132. [Link] [DOI:10.1006/jfls.2000.0329]
18. Karpouzian G, Librescu L. Comprehensive model of anisotropic composite aircraft wings suitable for aeroelastic analyses. Journal of Aircraft. 1994;31(3):703-712. [Link] [DOI:10.2514/3.46551]
19. Mazidi A, Fazelzadeh SA. Flutter of a swept aircraft wing with a powered engine. Journal of Aerospace Engineering. 2009;23(4):243-250. [Link] [DOI:10.1061/(ASCE)AS.1943-5525.0000037]
20. Golparvar H, Nasrollahzade M, Hosseinian A. Investigating the effects of sweep angles on the boundary dynamic instability using Peters pattern. 10th International Conferece of Iranian Aerospace Society, 1-3 March, 2011, Tehran, Iran. Tehran: Iranian Aerospace Society; 2011. [Persian] [Link]

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