Publication detail

Design of the Flying Airfoil Testbed

DANĚK, V. KOUŘIL, M. ŠOŠOVIČKA, R.

Original Title

Design of the Flying Airfoil Testbed

Type

conference paper

Language

English

Original Abstract

The paper concerns the design and possibility usage of the flying laboratory, based on the L-13 motor glider. It provides the primary analysis of its general conception and the way of measuring the wing sections. It also proposes the possibility of using the flying laboratory for measuring the performance and flight charcterisrtics.

Keywords

Aeronautics, Aerodynamics, Flight test, Airfoil

Authors

DANĚK, V.; KOUŘIL, M.; ŠOŠOVIČKA, R.

RIV year

2002

Released

21. 10. 1999

Publisher

Vojenský letecký technický skúšobný ústav Košice

Location

Košice

ISBN

80-7100-970-9

Book

Vedecko-technický rozvoj letectva a protivzdušnej obrany

Edition number

1.

Pages from

375

Pages to

379

Pages count

5

URL

LÚ FSI VUT v Brně

BibTex

@inproceedings{BUT10519,
  author="Vladimír {Daněk} and Martin {Kouřil} and Róbert {Šošovička}",
  title="Design of the Flying Airfoil Testbed",
  booktitle="Vedecko-technický rozvoj letectva a protivzdušnej obrany",
  year="1999",
  number="1.",
  pages="5",
  publisher="Vojenský letecký technický skúšobný ústav Košice",
  address="Košice",
  isbn="80-7100-970-9",
  url="LÚ FSI VUT v Brně"
}