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91 029 (0,32s)

Result

Aeroelastic Analysis and Experiment of an Airliner Half-Wing Model

The paper deals with aeroelastic analysis and experiments of the isolated half?wing of the research wind tunnel model EuRAM (European Research Aeroelastic Model) performed at VZLU in the frame of the projects ?Active Ae...

JU - Aeronautika, aerodynamika, letadla

  • 2007
  • Jx
Result

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 demonstrat...

JU - Aeronautika, aerodynamika, letadla

  • 2005
  • Jx
Result

X-DIA Demonstrator Aeroelastic Test

The paper deals with the tests of the X-DIA component aeroelastic demonstrator (the front part of the fuselage with the foreplane of the three plane jet transport aircraft) in the VZLU Prague....

JU - Aeronautika, aerodynamika, letadla

  • 2005
  • D
Result

Experimental aeroelastic investigation of models with one- and two degrees of freedom.

Two models for aeroelastic experiments were realized and partly tested. Models have one- and two-degrees of freedom, elastic properties of these models are changeable. It is possible to carry out simultaneous optical measurements of...

BK - Mechanika tekutin

  • 2003
  • D
Result

W-WING Aeroelastic Demonstrator Design Modification and Upgrade

W-WING is aeroelastic demonstrator representing a half-wing with the nacelle, engine, and propeller that is used for the experimental research of whirl flutter aeroelastic phenomenon. Two experimental campaigns w...

Aerospace engineering

  • 2024
  • D
  • Link
Result

Experimental Research into Whirl Flutter Aeroelastic Phenomenon

The paper is focused on the experimental research into the whirl flutter aeroelastic phenomenon. First, theoretical background on the whirl flutter and on its developments in the field is provided. The main part deals with the new <...

Aerospace engineering

  • 2023
  • D
Result

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 describes the aeroelastic response FE simulations and comparison of...

JU - Aeronautika, aerodynamika, letadla

  • 2005
  • D
Result

Reduced problem of non-linear aeroelastic stability and relevant post-critical states

This paper deals with the development of a uniform theory based simultaneously on theory and experiments which would cover known cases of aeroelastic instability and restabilisation due to non-linear and non-symmetrical terms....

JM - Inženýrské stavitelství

  • 2008
  • D
Result

Aeroelastic experiments with measurement of the kinematic properties based on optical methods

confirmed during an experiment performed on an aeroelastic experimental standA credible aeroelastic experiment deals with variables important for the description of dynamics of aeroelastic phenom...

BI - Akustika a kmity

  • 2015
  • Jx
  • Link
Result

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
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