Publication detail
Design of the Flying Airfoil Testbed
DANĚK, V. KOUŘIL, M. ŠOŠOVIČKA, R.
English title
Design of the Flying Airfoil Testbed
Type
Paper in proceedings (conference paper)
Language
en
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 in English
Aeronautics, Aerodynamics, Flight test, Airfoil
Released
1999-10-21
Publisher
Vojenský letecký technický skúšobný ústav Košice
Location
Košice
ISBN
80-7100-970-9
Book
Vedecko-technický rozvoj letectva a protivzdušnej obrany
Pages from–to
375–
Pages count
5
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"
}