Filtry
Optimization of the Commuter Aircraft Wing stiffness Characteristics Considering Requirement of Aeroelastic Stability at the Certification Speed
Paper deals with aeroelastic optimization. It gives a summary of theory with special regard to the aeroelasticity. Main part describes optimization of the aircraft wing stiffness characteristics to ensure the flutt...
JU - Aeronautika, aerodynamika, letadla
- 2007 •
- D
Rok uplatnění
D - Stať ve sborníku
Aeroelastic Simulations of the SADE FNG Smart Leading Edge ? Smart Single Slotted Flap High-lift Configuration
of aeroelastic efficiency of the FNG high-lift configuration, investigated within the EU was produced by VZLU. This model was then used for further structural aeroelastic optimisation (FOI) and an evaluation of the aeroelastic<...
JU - Aeronautika, aerodynamika, letadla
- 2014 •
- D •
- Odkaz
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
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. Paper is focused to design, analysis and manufacturing of new composite foreplanes, FE analyses of the X-DIA Component Model (static
JU - Aeronautika, aerodynamika, letadla
- 2005 •
- 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)
Aeroelastic model of a morphing wing for control design and optimization
Two dimensional unsteady aerodynamic model in time domain is derived using approximated Wagner function. Strip theory is used to obtain three dimensional aeroelastic model of high aspect ratio morphing wing in state space form. Several simul...
Applied mechanics
- 2021 •
- D •
- Odkaz
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
Aeroelastic Test of the Three Surface demonstrator Front Fuselage and Foreplane Component Model
Component Model (static aeroelasticity, flutter, dynamic responses) and optimizationSubmitted paper deals with the 3-surface X-DIA aeroelastic research demonstrator component wind tunnel tests. First part of the paper is f...
JU - Aeronautika, aerodynamika, letadla
- 2008 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Aeroelastic Analysis of Twin Turboprop Utility Aircraft
This paper deals with aeroelastic certification analyses of the new generation, static aeroelastic analyses (control reversal and divergence), modal analyses parameters are presented. Furthermore the preparation of the GVT, i.e. the...
JU - Aeronautika, aerodynamika, letadla
- 2011 •
- Jx •
- Odkaz
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Výsledek na webu
Aeroelastic Analysis of New Generation Czech Twin Turboprop Utility Aircraft
This paper deals with aeroelastic certification analyses of the EV-55 ?Outback blocks of analyses follows afterwards. It includes static aeroelastic analyses the preparation of the GVT, i.e. the optimization of the exciter ...
JU - Aeronautika, aerodynamika, letadla
- 2011 •
- Jx •
- Odkaz
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Výsledek na webu
Aeroelasticity Aircraft certification
Aeroelasticity Aircraft certification Aeroelasticity Aircraft certification Aeroelasticity Aircraft certification Aeroelasticity Aircraft certification......
JU - Aeronautika, aerodynamika, letadla
- 2003 •
- X
Rok uplatnění
X - Nezařazeno
Procedure of the small aircraft aeroelastic certification for static aeroelasticity
Procedure of the static aeroelastic analyses of the small transport aircraft. Certification analyses procedure regarding FAR 23, JAR 23, CS 23 airworthiness regulations. Usable for aeroelastic certification of new aircraft structure...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- X
Rok uplatnění
X - Nezařazeno
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