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The effect of sweep angle on the limit cycle oscillations of aircraft wings
Seher Eken
*
,
Metin Orhan Kaya
*
Corresponding author for this work
Department of Astronautical Engineering
Department of Aeronautical Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
3
Citations (Scopus)
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Dive into the research topics of 'The effect of sweep angle on the limit cycle oscillations of aircraft wings'. Together they form a unique fingerprint.
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Keyphrases
Aircraft Wing
100%
Sweep Angle
100%
Limit Cycle Oscillation
100%
Strip Theory
66%
Two-degree-of-freedom
33%
Aeroelasticity
33%
Cantilever
33%
Mode Shape
33%
Flutter Analysis
33%
Incompressible Flow
33%
Cantilever Beam
33%
Swept Wing
33%
Unsteady Aerodynamics
33%
Flutter Boundary
33%
Cubic Nonlinearity
33%
Harmonic Balance Method
33%
Swept-back Wing
33%
Engineering
Wings
100%
Limit Cycle
100%
Sweep Angle
100%
Strip Theory
66%
Two Degree of Freedom
33%
Mode Shape
33%
Cantilever Beam
33%
Incompressible Flow
33%
Harmonic Balance
33%
Swept Wings
33%
Nonlinearity
33%