Publication detail

Response of light aircraft under gust loads

CHUDÝ, P.

Original Title

Response of light aircraft under gust loads

Type

journal article - other

Language

English

Original Abstract

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.

Key words in English

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

Authors

CHUDÝ, P.

RIV year

2004

Released

6. 6. 2004

Publisher

The Czech Technical University in Prague Publishing House

Location

Prague

ISBN

1210-2709

Book

Acta Polytechnica

Edition

2004

Edition number

2/2004

ISBN

1210-2709

Periodical

Acta Polytechnica

Number

2

State

Czech Republic

Pages from

97

Pages to

102

Pages count

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"
}