Publication detail

Very light airplane longitudinal dynamic stability analysis

DANĚK, V.

Czech title

Analýza podélné dynamické stability velmi lehkého letounu

English title

Very light airplane longitudinal dynamic stability analysis

Type

journal article - other

Language

en

Original abstract

A linearized analytic model of general longitudinal movement of airplane is discussed. Linearized deviation equations of motion, derived in stability axes system, are applied to the parametric analysis of airplane's longitudinal dynamic stability under arbitrary symetric flight conditions.

Czech abstract

Rozebírá se linearizovaný výpočtový model podélného pohybu letounu. Na základě linearizovaných pohybových rovnic, zapsaných ve stabilitní souřadnicové soustavě, se provádí parametrická analýza podélné dynamické stability letounu pro libovolný symetrický režim letu.

English abstract

A linearized analytic model of general longitudinal movement of airplane is discussed. Linearized deviation equations of motion, derived in stability axes system, are applied to the parametric analysis of airplane's longitudinal dynamic stability under arbitrary symetric flight conditions.

Keywords in English

Aerodynamics, Flight, Dynamic stability

RIV year

2002

Released

01.10.2002

ISSN

0002-2667

Journal

Aircraft Engineering and Aerospace Technology: An International Journal

Volume

2002

Number

5

Pages count

6

BIBTEX


@article{BUT41041,
  author="Vladimír {Daněk},
  title="Very light airplane longitudinal dynamic stability analysis",
  journal="Aircraft Engineering and Aerospace Technology: An International Journal",
  year="2002",
  volume="2002",
  number="5",
  month="October",
  issn="0002-2667"
}