Publication detail

VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS

JEBÁČEK, I.

Original Title

VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS

Type

journal article - other

Language

English

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

Measurement, lift curve slope, in flight

Authors

JEBÁČEK, I.

RIV year

2010

Released

18. 3. 2010

Publisher

Czech Aerospace Manufacturers Association

Location

Praha

ISBN

1211-877X

Periodical

Letecký zpravodaj

Year of study

2010

Number

1

State

Czech Republic

Pages from

60

Pages to

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"
}