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JEBÁČEK, I.
Originální název
VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS
Typ
článek v časopise - ostatní, Jost
Jazyk
angličtina
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
Measurement, lift curve slope, in flight
Autoři
Rok RIV
2010
Vydáno
18. 3. 2010
Nakladatel
Czech Aerospace Manufacturers Association
Místo
Praha
ISSN
1211-877X
Periodikum
Letecký zpravodaj
Ročník
Číslo
1
Stát
Česká republika
Strany od
60
Strany do
62
Strany počet
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" }