Detail publikace

Hydraulic booster dynamic properties of aircraft control system.

KAMENÍK, L.TŘETINA, K.

Anglický název

Hydraulic booster dynamic properties of aircraft control system.

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

This article focuses on the dynamic properties of the booster in the hydraulic system of the aircraft control. The analysis has been made with the use of physical-analytic method of the description of the operation of the booster and an experimental measuring has been added.

Klíčová slova anglicky

aircraft control system, hydraulic booster, dynamic properties

Vydáno

2007-02-15

Nakladatel

Czech Aerospace Manufactures Association

Místo

AVL, Prague

ISSN

1211-877X

Časopis

Letecký zpravodaj

Ročník

2007

Číslo

2

Strany od–do

28–32

Počet stran

4

BIBTEX


@article{BUT49904,
  author="KAMENÍK, L. and TŘETINA, K.",
  title="Hydraulic booster dynamic properties of aircraft control system.",
  journal="Letecký zpravodaj",
  year="2007",
  volume="2007",
  number="2",
  pages="28--32",
  issn="1211-877X"
}