Detail publikace

COMPUTATIONAL DYNAMICS OF A LIGHT AIRPLANE

CHUDÝ, P.

Originální název

COMPUTATIONAL DYNAMICS OF A LIGHT AIRPLANE

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

This paper presents the work performed by the Institute of Aerospace Engineering, Brno University of Technology. Project’s main purpose was to compare the results obtained from complex numerical simulation and analytical solutions of airplane’s aeroelastic response. Numerical simulations provide a complex description of the analyzed dynamic processes and monitoring of selected quantities in the time domain. This represents a tool for a visual qualification of the investigated process. Utilization of a simplified beam-stick model represents an industrial standard in the field of computational aeroelasticity/flight mechanics. The need for complex aeroelastic simulations leads to a concept of an advanced aeroelastic model that integrates advanced 3D dynamic part (model) with proven aerodynamic theory.

Klíčová slova v angličtině

Computational Aeroelasticity, Computational Flight Mechanics, Dynamic Response Estimation, Finite Element Model, Unsteady Aerodynamics, Advanced modeling techniques, Flying Qualities

Autoři

CHUDÝ, P.

Rok RIV

2004

Vydáno

9. 12. 2004

Nakladatel

Vilnius "Technika"

Místo

Vilnius, Lithuania

ISBN

9986-05-795-7

Kniha

Aviation 2004

Strany od

8

Strany do

13

Strany počet

6

BibTex

@inproceedings{BUT17079,
  author="Peter {Chudý} and Vladimír {Daněk}",
  title="COMPUTATIONAL DYNAMICS OF A LIGHT AIRPLANE",
  booktitle="Aviation 2004",
  year="2004",
  number="Vol IX, No 1",
  pages="6",
  publisher="Vilnius {"}Technika{"}",
  address="Vilnius, Lithuania",
  isbn="9986-05-795-7"
}