Detail publikace

Response of light aircraft under gust loads

CHUDÝ, P.

Originální název

Response of light aircraft under gust loads

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

Originální abstrakt

In general, there are two methods widely accepted by the aeronautical authorities. Both of them are implemented in the world leading sets of aeronautical safety requirements. The deterministic method describes the ‘worst case’ atmospheric gust approach. The nature of the gust field is reduced to a form of one dominant discrete gust with closer shape specification. The second approach belongs to the family of statistical methods. The atmosphere is described by the power spectral density function and transforms the problem from the time to a frequency domain. For both methods a set of gust velocities for specific flight conditions has been defined.

Klíčová slova v angličtině

computational aeroelasticity, gust loading, dynamic response estimation, finite element model, unsteady aerodynamics, advanced modeling techniques

Autoři

CHUDÝ, P.

Rok RIV

2004

Vydáno

6. 6. 2004

Nakladatel

The Czech Technical University in Prague Publishing House

Místo

Prague

ISBN

1210-2709

Kniha

Acta Polytechnica

Edice

2004

Číslo edice

2/2004

ISSN

1210-2709

Periodikum

Acta Polytechnica

Číslo

2

Stát

Česká republika

Strany od

97

Strany do

102

Strany počet

6

BibTex

@article{BUT42402,
  author="Peter {Chudý}",
  title="Response of light aircraft under gust loads",
  journal="Acta Polytechnica",
  year="2004",
  number="2",
  pages="6",
  issn="1210-2709"
}