Static Aeroelastic Effects on a Transonic Indicial Response Wing Flutter Calculation

Static Aeroelastic Effects on a Transonic Indicial Response Wing Flutter Calculation

Kolonay and Yang demonstrate the effect of static aeroelastic equilibrium on a three-dimensional transonic small disturbance indicial response method wing flutter analysis.

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Veröffentlicht in:Journal of aircraft 1998-03, Vol.35 (2), p.339-341
Hauptverfasser: Kolonay, R. M, Yang, Henry T. Y
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Aircraft
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Physics
Solid mechanics
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
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Beschreibung
Zusammenfassung:Kolonay and Yang demonstrate the effect of static aeroelastic equilibrium on a three-dimensional transonic small disturbance indicial response method wing flutter analysis.
ISSN:0021-8669
1533-3868
DOI:10.2514/2.7578