doc. Ing. Ivo Jebáček, Ph.D.
E-mail:   jebacek@fme.vutbr.cz 
Dept.:   Institute of Aerospace Engineering
Dept. of Aerospace Technology
Position:   Associate Professor

Education and academic qualification

  • 1996 - 1999 Brno University of Technology, Faculty of Mechanical Engineering
  • Specialization: Design and Process Engineering – postgraduate course
  • 1991 - 1996 Brno University of Technology, Faculty of Mechanical Engineering
  • Specialization: Aeronautical Engineering

Career overview

  • 2002 – Lecturer, Institute of Aerospace Engineering FME BUT,
  • 1999 – 2002 Asistent, Institute of Aerospace Engineering FME BUT,
  • 1998 – 1999 Technical worker, Institute of Aerospace Engineering FME BUT,

Pedagogic activities

  • Aircraft testing (OZK)
  • Diploma Project (M2325) (OD5)
  • Diploma Seminar (M2325) (ODS)

Scientific activities

  • 2002 – Grant project leader č. FP 320051, Measurement of balancing loading of TL-2000 Sting aircraft
  • 2001 – Grant project leader č. FP 310046, In flight measurement of horizontal tail loading of a small aircraft
  • 1999 – Grant project leader č. FP 380038, Sensors calibration for in flight measurement of horizontal tail loading of a small aircraft
  • 1998 – Grant project leader č. FV 380009/98, In flight measurement of strength values, performance and flight characteristic

Prizing by scientific community

  • In 1996 awarded prize of Minister of Education

Sum of other citations (without self-citations)

5

Supervised courses:

Publications:

  • JEBÁČEK, I.; VANĚK, F.:
    Main landing gear of the L410 NG aircraft, Lú, VUT v Brně
    summary research report - contract. research
  • JEBÁČEK, I.; VANĚK, F.:
    Static strength test of Stemme TSA-M/S6-RT outer wing structure, LÚ, VUT v Brně
    summary research report - contract. research
  • AUGUSTIN, P.; JEBÁČEK, I.:
    STATIC AND FATIGUE TESTS OF 240%-CFRP-TUBES CONNECTIONS, LÚ, VUT v Brně
    summary research report - contract. research
  • JEBÁČEK, I.; HORÁK, M.:
    Possibilities and methods of in-flight loading measurement,
    AVIATION, Vol.16, (2012), No.2, pp.47-50, ISSN 1648-7788, Vilnius Gediminas Technical University
    journal article - other
  • AUGUSTIN, P.; JEBÁČEK, I.:
    METHODOLOGY OF STATIC AND FATIGUE TESTS OF 240%-CFRP-TUBES CONNECTIONS, LÚ, VUT v Brně
    summary research report - contract. research
  • JEBÁČEK, I.:
    MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST,
    27th Congress of International Council of Aeronautical Sciences, pp.1-7, ISBN 978-0-9565333-0-2, (2010), Optimage Ltd.
    conference paper
    akce: 27th Congress of the International Council of the Aeronautical Sciences, NICE, 20.09.2010-23.09.2010
  • JEBÁČEK, I.:
    VERIFICATION OF AERODYNAMIC CHARACTERISTIC BY IN FLIGHT MEASUREMENTS,
    Letecký zpravodaj, Vol.2010, (2010), No.1, pp.60-62, ISSN 1211-877X, Czech Aerospace Manufacturers Association
    journal article - other
  • JEBÁČEK, I.:
    Návrh a realizace moderních metod zkoušení leteckých konstrukcí
    habilitation thesis
  • JEBÁČEK, I.:
    FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS,
    AVIATION Research Journal of Vilnius Gediminas Technical University, Vol.2009, (2009), No.13, pp.26-33, ISSN 1822-4180, Vilnius Gediminas Technical University
    journal article - other
    akce: Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education 2008, Brno, Hotel Continental, 16.10.2008-17.10.2008

List of publications at Portal BUT

Abstracts of most important papers:

  • JEBÁČEK, I.; Šplíchal, J.:
    Composite specimens, Lú, VUT v Brně
    summary research report - contract. research
    Tests of composites samples and material qualification. Material will be used for a new aircraft prototype
  • JEBÁČEK, I.; VANĚK, F.:
    Main landing gear of the L410 NG aircraft, Lú, VUT v Brně
    summary research report - contract. research
    Drop tests with spinning wheel and measuring the vertical and horizontal forces
  • JEBÁČEK, I.; VANĚK, F.:
    Static strength test of Stemme TSA-M/S6-RT outer wing structure, LÚ, VUT v Brně
    summary research report - contract. research
    Static strength test of the outer wing aircraft to establish wing load capacity
  • JEBÁČEK, I.; HORÁK, M.:
    Possibilities and methods of in-flight loading measurement,
    AVIATION, Vol.16, (2012), No.2, pp.47-50, ISSN 1648-7788, Vilnius Gediminas Technical University
    journal article - other
    This article provides information about in-flight measurement of a small sport aircraft. Firstly the strain gauges were installed into the wing structure and then the calibration procedures were done. After the calculation of strain gauge coefficients the equations for calculating of bending moments and other variables were established. The data acquisition system was installed into the aircraft for measurement responses from strain gauges and other variables as speed, altitude, load factor and temperature. Many flights were performed with this way equipped aircraft and after that the recorded data were analyzed and those results were compared with the calculation and with the static strength tests performed before.
  • JEBÁČEK, I.:
    MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST,
    27th Congress of International Council of Aeronautical Sciences, pp.1-7, ISBN 978-0-9565333-0-2, (2010), Optimage Ltd.
    conference paper
    akce: 27th Congress of the International Council of the Aeronautical Sciences, NICE, 20.09.2010-23.09.2010
    The goal of measurement was to set curves of bending moment on the wing of a small aircraft and establishing of the strain in dependence on a flight conditions. The results were used for design of the fatigue test of the connection between the center wing and outer wing.