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Information Journal Paper

Title

DYNAMIC INSTABILITY ANALYSIS OF A SWEPT WING IN TIME - DOMAIN

Pages

  93-106

Abstract

 In this paper linear aeroelastic analysis of a SWEPT WING with two degrees of freedom in an incompressible flow is investigated in time - domain. The equations of the motion of an elastic wing are derived from Lagrange’s equations in time - domain. The wing is modeled as a cantilever beam rigidly connected to the root. Considering assumed modes of cantilever beam, aerodynamic forces and moments acting on the wing are derived using strip - theory in an unsteady incompressible potential fluid flow. The governing aeroelastic equations of the system have been introduced in dimensionless form. These equations are solved via a numerical method. Comparisons between obtained results and both available experimental data and the results of some cited references indicate a close agreement.

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    Cite

    APA: Copy

    GHADIRI, B., RAZI, M., & HAMIDI, S.. (2010). DYNAMIC INSTABILITY ANALYSIS OF A SWEPT WING IN TIME - DOMAIN. MODARES TECHNICAL AND ENGINEERING, -(37 (SPECIAL ISSUE ON MECHANICAL ENGINEERING)), 93-106. SID. https://sid.ir/paper/24997/en

    Vancouver: Copy

    GHADIRI B., RAZI M., HAMIDI S.. DYNAMIC INSTABILITY ANALYSIS OF A SWEPT WING IN TIME - DOMAIN. MODARES TECHNICAL AND ENGINEERING[Internet]. 2010;-(37 (SPECIAL ISSUE ON MECHANICAL ENGINEERING)):93-106. Available from: https://sid.ir/paper/24997/en

    IEEE: Copy

    B. GHADIRI, M. RAZI, and S. HAMIDI, “DYNAMIC INSTABILITY ANALYSIS OF A SWEPT WING IN TIME - DOMAIN,” MODARES TECHNICAL AND ENGINEERING, vol. -, no. 37 (SPECIAL ISSUE ON MECHANICAL ENGINEERING), pp. 93–106, 2010, [Online]. Available: https://sid.ir/paper/24997/en

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