Detail publikace

The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

KOUŘIL, M. JEBÁČEK, I. Prokš, M.

Anglický název

The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

The dynamic stability control presents one of the important parts of flight characteristics analysis of design atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have a great influence on the final aircraft appearance. The suitability of proposed aircraft design and possible modifications will appear just during the flight tests. The results of flight tests are used for the verification of applied theory and for the verification of designed aircraft stability and control as well. This paper presents the issue of flight measurement and theory calculations of longitudinal dynamic stability. It is dealing in detail with comparison of performed flight measurements and computations. The aircraft, mainly supporting this research, is the two-seat all-metal motor glider L-13 SE Vivat.

Klíčová slova anglicky

Aerodynamics, mechanics of flight, flight-tests, dynamic stability, flight characteristics

Vydáno

2003-11-21

Nakladatel

VZLÚ, a.s.

Místo

Praha

ISSN

1211-877X

Kniha

Letecký zpravodaj

Časopis

Letecký zpravodaj

Ročník

2003

Číslo

3

Strany od–do

6–

Počet stran

4

BIBTEX


@article{BUT41950,
  author="Martin {Kouřil} and Ivo {Jebáček}",
  title="The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft",
  journal="Letecký zpravodaj",
  year="2003",
  volume="2003",
  number="3",
  pages="4",
  issn="1211-877X"
}