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Flutter resistance of wing for VL-3 LSA airplane with aileron v.2023
The analysis of an aileron mass characteristic influence to the flutter velocity.
Aerospace engineering
- 2023 •
- O
Rok uplatnění
O - Ostatní výsledky
Assessment of Aileron Tab Installation Influence to Aircraft Flutter Characteristics
This paper deals with the aileron flutter of the ultra-light aircraft. It gives an assessment of influence of the retrofitting of the tab regarding the aircraft aileron flutter characteristics. The necessary actuat...
JU - Aeronautika, aerodynamika, letadla
- 2014 •
- D •
- Link
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
Assessment of Aileron Tab Installation Influence on Light Sport Aircraft Flutter Characteristics
This paper deals with the aileron flutter of the light sport aircraft. It gives an assessment of the influence of the retrofitting of the tab with regard to the aircraft aileron flutter characteristics. The necessa...
JU - Aeronautika, aerodynamika, letadla
- 2013 •
- Jx •
- Link
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Výsledek na webu
Methodology of Aircraft Structure Finite Model Preparation by Means of Optimization-based Approach with Special Regard to the Ultra-light Aircraft Category
aircraft wing model example. As an example task, the study of influence of the aileron tab retrofitting to the aileron flutter stability is performed....
JU - Aeronautika, aerodynamika, letadla
- 2009 •
- NmetC
Rok uplatnění
NmetC - Metodiky certifikované oprávněným orgánem
Aeroelasticity analysis of the wing UL-39
This paper deals with computation of modal and flutter characteristic, investigating ailerons effectiveness and determine torsion divergence critical velocity at right half-wing of the aircraft UL-39.The problems are solved in FEM s...
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- D
Rok uplatnění
D - Stať ve sborníku
Adaptive control design for the aeroelastic wing
demonstrate the possibilities of such a controller for active flutter suppression on the linear parameter-varying (LPV) servoaeroelastic wing model with two ailerons....
Automation and control systems
- 2021 •
- D •
- Link
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
Distributed control for a morphing wing with a macro fiber composite actuator
of aeroelastic structures like wings or ailerons. This instability called flutter occurs above the critical (flutter) speed where at least one of the modes is no longer specifically the flexible wing flutter....
Automation and control systems
- 2018 •
- O
Rok uplatnění
O - Ostatní výsledky
Analysis of the Airliner Half-wing Aeroelastic Model
redistributions on the deformed structure and flutter stability were compared excitation by deflection of non-typically positioned control surface ? tip aileron....
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- D
Rok uplatnění
D - Stať ve sborníku
Numerical simulation of influence of a gap between the main lifting surface and the aileron on aeroelastic behavior of an airfoil
the elastic axis, oscillations in the vertical and rotation of the aileron around the axis of the gap between the main lifting surface and the aileron....
BI - Akustika a kmity
- 2012 •
- D
Rok uplatnění
D - Stať ve sborníku
Numerical Simulation of Influence of a Gap between the Main Lifting Surface and the Aileron on Aeroelastic Behaviour of an Airfoil
of the aileron around the axis. The finite element (FE) solution of the Navier - Stokes damping, limit cycle oscillations (LCO) and the flutter instability of the airfoil the main lifting surface and the aileron....
BI - Akustika a kmity
- 2012 •
- D
Rok uplatnění
D - Stať ve sborníku
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