Publication detail

VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS

JEBÁČEK, I.

English title

VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

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.

Keywords in English

Measurement, lift curve slope, in flight

Released

2010-03-18

Publisher

Czech Aerospace Manufacturers Association

Location

Praha

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2010

Number

1

Pages from–to

60–62

Pages count

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"
}