DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS

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GHASEMI ASL R.; GHADIRI B.

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Journal: ESTEGHLAL Year:2007 | Volume:26 | Issue:1 Page(s): 197-207

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Information Journal Paper

Title

DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS

Author(s)

GHASEMI ASL R. | GHADIRI B. | Issue Writer Certificate

Keywords

DYNAMIC INSTABILITY OF WINGQ3

FLUTTERQ2

AEROELASTICITYQ1

ASSUMED MODEQ3

V-G METHODQ3

Abstract

In this paper, the equation of motion of an elastic 2 DoF wing model has been derived using Lagrange’s method. The aerodynamic loads on the wing were calculated via the Strip-Theory and the effect of compressibility was included. Wing deflections due to bending and twist motions were determined using the Assume-Mode method. The aeroelastic equations were solved numerically using the V-G METHOD. The results obtained for different types of wings were in good agreement with experimental data.

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APA: Copy

GHASEMI ASL, R., & GHADIRI, B.. (2007). DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS. ESTEGHLAL, 26(1), 197-207. SID. https://sid.ir/paper/6007/en

Vancouver: Copy

GHASEMI ASL R., GHADIRI B.. DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS. ESTEGHLAL[Internet]. 2007;26(1):197-207. Available from: https://sid.ir/paper/6007/en

IEEE: Copy

R. GHASEMI ASL, and B. GHADIRI, “DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS,” ESTEGHLAL, vol. 26, no. 1, pp. 197–207, 2007, [Online]. Available: https://sid.ir/paper/6007/en

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