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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 ...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- X
Rok uplatnění
X - Nezařazeno
Methodology of the small transport aircraft aeroelastic certification ? static aeroelasticity
Submitted methodology provides procedures for small transport aircraft aeroelastic certification in the field of static aeroelasticity. It deals with procedures of aeroelastic certification calculations according a...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- X
Rok uplatnění
X - Nezařazeno
Static Aeroelasticity Results Plotter
Software for evaluation a results FEM analysis using software MSC.Nastran. That are results of static aeroelasticity problems (SOL 144) as control reversal and torsion divergence....
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- R
Rok uplatnění
R - Software
High-fidelity static aeroelastic simulations of the common research model
of high-fidelity aeroelastic simulation tool. Currently, it allows to perform static impact the aeroelastic effects, which can be more easily excited by rigid body motions than in case of stiffer structures. The potential ...
Aerospace engineering
- 2020 •
- D •
- Link
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 optimization the stiffness, modal and mainly aeroelastic static and dynamic wind tunnel testsSubmitted paper deals with the 3-surface X-DIA <...
JU - Aeronautika, aerodynamika, letadla
- 2008 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
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 (stati...
JU - Aeronautika, aerodynamika, letadla
- 2005 •
- 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 (s...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
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 aeroelastic ...
Aerospace engineering
- 2022 •
- D
Rok uplatnění
D - Stať ve sborníku
Aeroelastic Model
Use of detailed structural models was previously limited to cases of static or dynamic load tests. These have been compared to experimentally obtained data and calibrated. A generally accepted illustration of classical aeronautical structure...
JU - Aeronautika, aerodynamika, letadla
- 2004 •
- Vx
Rok uplatnění
Vx - Nezařazeno - Výzkumná zpráva obsahující utajované informace (takový výsledek lze do RIV vložit pouze v případě, že zpráva obsahuje utajované informace a pole R12 = U), nebo souhrnná výzkumná zpráva
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