The transonic dip in aeroelastic divergence speed -- An explicit formula

DOI10.1016/J.JFRANKLIN.2011.10.004zbMath1254.93080OpenAlexW2054828108MaRDI QIDQ1926327

A. V. Balakrishnan, Amjad M. Tuffaha

Publication date: 28 December 2012

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2011.10.004

zbMATH Keywords

finite element methodMach numberangle of attackcontinuum modelsdivergence speedcurvilinear finite differencedependence on wing cambernonzero camberPossio integral equationtransonic dip in aeroelastic divergencewing thickness ratio

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Linear systems in control theory (93C05) Eigenvalue problems (93B60) Control/observation systems governed by functional relations other than differential equations (such as hybrid and switching systems) (93C30)

Related Items (1)

Static stability analysis of a thin plate with a fixed trailing edge in axial subsonic flow: Possio integral equation approach

Cites Work

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• State space representation of flexible structure dynamics in air flow
• A novel technique for optimal placement of piezoelectric actuators on smart structures
• Subsonic flutter suppression using self-straining actuators
• Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model.
• Elastic plate in gas flow: Reducing from anisotropy to orthotropy

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