Detail publikace
VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS
JEBÁČEK, I.
Anglický název
VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS
Typ
Článek recenzovaný mimo WoS a Scopus
Jazyk
en
Originální abstrakt
This paper describes the measurements of the lift curve slope of ultra light aircraft KP-2U QWL. The lift curve slope was obtained by a pitot-static probe installed on the wing of the aircraft. Basic parameters such as, speed, altitude and temperature, were recorded by the data acquisition system ESAM Trveller Static. Then the recorded data was analyzed. The result of this analysis was the lift curve slope of the aircraft. The measured lift curve slope was compared with the computed result.
Klíčová slova anglicky
Measurement, lift curve slope, in flight
Vydáno
2010-03-18
Nakladatel
Czech Aerospace Manufacturers Association
Místo
Praha
ISSN
1211-877X
Časopis
Letecký zpravodaj
Ročník
2010
Číslo
1
Strany od–do
60–62
Počet stran
2
BIBTEX
@article{BUT50064,
author="Ivo {Jebáček}",
title="VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS",
journal="Letecký zpravodaj",
year="2010",
volume="2010",
number="1",
pages="60--62",
issn="1211-877X"
}