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Procedure of aeroelastic response to the control surface excitation analysis
Procedure of the aeroelastic response to the control surface aerodynamic excitation analysis. analysis is performed by means of the NASTRAN program system. Excitation signal may be harmonic or general (in time domain). Procedure all...
JU - Aeronautika, aerodynamika, letadla
- 2005 •
- X
Rok uplatnění
X - Nezařazeno
Aeroelastic Response Analysis of the X-DIA Demonstrator Component Model
The submitted paper desribes aeroelastic response simulations carried out on the X-DIA, three surface aeroelastic demonstrator component model (front fuselage + foreplane). Analytical results were compared with results of d...
JU - Aeronautika, aerodynamika, letadla
- 2005 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Landing Shock Aeroelastic Response Analysis of EV 55M Utility Aircraft
The paper deals with the EV-55M aircraft landing shock aeroelastic response analysis. The analysis was performed as a part of the aircraft certification in order flight envelope and the regulation statements. The modal transient
JU - Aeronautika, aerodynamika, letadla
- 2012 •
- Jx •
- Link
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
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Analysis of turboprop aircraft aeroelastic response including effects of powerplant rotating mass
Submitted paper is focused on aeroelastic response analysis of a turboprop aircraft structure including the aerodynamic and dynamic effects of rotating masses with respect to stability (whirl flutter). Nevertheless, the aeroelas...
Aerospace engineering
- 2022 •
- D
Rok uplatnění
D - Stať ve sborníku
Dynamic Response Analysis and Experimental Validation of the X-DIA Demonstrator Component Model
Submitted paper deals with the X-DIA three surface aeroelastic demonstrator component model relating activities. Paper is focused to the preparation and realization of the test programme (stiffness tests, modal tests, wind tunnel tests). Sep...
JU - Aeronautika, aerodynamika, letadla
- 2005 •
- D
Rok uplatnění
D - Stať ve sborníku
Aeroelastic Response of a Light Aircraft
Considerable evidence can be found indicating that most of the severe gusts occur more or less as individual gusts. Purpose of the project was to compare the results obtained from classical analytical solutions and a complex numerical simulation of a...
JU - Aeronautika, aerodynamika, letadla
- 2004 •
- D
Rok uplatnění
D - Stať ve sborníku
Aeroelastic simulations with application of CFD method with moving grid
of aeroelastic response ofaircraft structural parts of classical conception. Together with development of the field of aeroelasticity and increasing performance of the computational hardware there is coming possibility to ...
JU - Aeronautika, aerodynamika, letadla
- 2007 •
- D
Rok uplatnění
D - Stať ve sborníku
Analysis of the Airliner Half-wing Aeroelastic Model
The submitted paper deals with analytical calculations, mainly aeroelastic, performed on the half-wing model of the aeroelastic research demonstrator EuRAM. Results of calculations of stiffness characteristics, modal characteristics...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- D
Rok uplatnění
D - Stať ve sborníku
X-DIA Demonstrator Aeroelastic Test ? Design, Analysis And Model Wind Tunnel Support Tuning
Submitted paper deals with preparation of the X-DIA aeroelastic demonstrator component wind tunnel tests. The paper is focused on design, analysis and manufacturing of new composite foreplanes, FE analyses of the X-DIA Component Model (stati...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Numerical and experimental solution of non-linear aeroelastic response of a bridge girder
Analysis of the bridge girder under self-excited load is performed numericaly and experimentally.
JN - Stavebnictví
- 2008 •
- D
Rok uplatnění
D - Stať ve sborníku
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