
aeroelasticity
Sign in to savethumb|NASA testing a scale model Lockheed L-188 Electra|Lockheed Electra in a wind tunnel for flutter
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- Aeroelasticity
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Article
16 sectionsContents
- History
- Static aeroelasticity
- Divergence
- Control reversal
- Dynamic aeroelasticity
- Aeroservoelasticity
- Propeller whirl flutter
- Transonic aeroelasticity
- Buffeting
- Prediction and cure
- Media
- Notable aeroelastic failures
- See also
- References
- Further reading
- External links
thumb|NASA testing a scale model Lockheed L-188 Electra|Lockheed Electra in a wind tunnel for flutter
Aeroelasticity is the branch of physics and engineering studying the interactions between the inertial, elastic, and aerodynamic forces occurring while an elastic body is exposed to a fluid flow. The study of aeroelasticity may be broadly classified into two fields: static aeroelasticity dealing with the static or steady state response of an elastic body to a fluid flow, and dynamic aeroelasticity dealing with the body's dynamic (typically vibrational) response.