Publications

• 2023

  HÁJEK, T.; GRIM, R.; POPELA, R. IMPLEMENTATION STUDY OF A PASSIVE SAFETY FEATURE IN THE RESCUE SYSTEMS OF SMALL AIRCRAFTS. AVIATION, 2023, vol. 27, no. 3, p. 187-196. ISSN: 1648-7788.
  Detail | WWW | Full text in the Digital Library

  GRIM, R.; POPELA, R.; JEBÁČEK, I.; HORÁK, M.; ŠPLÍCHAL, J. Determination of the Parachute Harness Critical Load Based on Load Distribution into Individual Straps with Respect of the Skydiver’s Body Position. Aerospace, 2023, vol. 10, no. 1, p. 1-18. ISSN: 2226-4310.
  Detail | WWW | Full text in the Digital Library

  LAZAR, V.; MAŠEK, J.; POPELA, R.; JEBÁČEK, I. Determination of thermal contact resistance in thermo-vacuum chamber experiments. In Proceedings of the International Astronautical Congress, IAC. Proceedings of the International Astronautical Congress, IAC. Baku, Azerbaijan: International Astronautical Federation, 2023. ISSN: 0074-1795.
  Detail | WWW

• 2022

  MAŠEK, J.; LÖFFELMANN, F.; POPELA, R.; KUBÍK, P.; ŠEBEK, F.; KOUTNÝ, D.; MALÝ, M.; PANTĚLEJEV, L.; PAMBAGUIAN, L. Additive manufacturing capabilities for heat switch technology: Key challenges & knowledge gaps. Lille, Francie: EUCASS association, 2022. p. 1-15.
  Detail | WWW | Full text in the Digital Library

  BARTONĚK, J.; LAZAR, V.; MALANÍK, P.; RYDLO, Š.; LÁZNIČKA, T.; POPELA, R.; DRUCKMÜLLER, M. Low Earth Orbit determination in small satellite mission proposal for corona observation of close solar surface region. ACTA ASTRONAUTICA, 2022, vol. 203, no. Feb. 2023, p. 202-213. ISSN: 0094-5765.
  Detail | WWW

• 2020

  POPELA, R. Moon Drone. 2020.
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• 2018

  MAŠEK, J.; KOUTNÝ, D.; POPELA, R. Thermal conductivity of Cu7.2Ni1.8Si1Cr Copper alloy produced via SLM and ability of thin-wall structure fabrication. In 13th Research and Education in Aircraft Design Conference. READ 2018, Brno, ČR: Brno University of Technology, 2018. p. 119-129. ISBN: 978-80-214-5696-9.
  Detail | WWW

• 2015

  PEJCHAR, J.; DANIEL, M.; POPELA, R. Mars probe soft landing test in the Earth conditions. Engineering mechanics 2015 - Extended abstracts. 21st International conference May 11-14, 2015, Svratka, Czech Republic. Extended abstracts. Česká republika: Academy of Sciences of the Czech Republic, v.v.i., 2015. p. 226-227. ISBN: 978-80-86246-42- 0.
  Detail | WWW

  ZIKMUND, P.; POPELA, R. Airliner- UAV Flight Formation in Climb Regime. World Academy of Science, Engineering and Technology, 2015, vol. 9, no. 10, p. 631-636. ISSN: 1307- 6892.
  Detail | WWW

  PEJCHAR, J.; DANIEL, M.; POPELA, R. Mars probe soft landing test in the Earth conditions. Svratka, ČR: 2015.
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• 2014

  FAENZA, M.; MORETTO, F.; TIJSTERMAN, R.; DVOŘÁK, P.; POPELA, R.; PETRONIO, D.; PAVARIN, D. Experimental Characterization of a Cavitating Pintle Valve with H2O2. In Space Propulsion Conference 2014 Proceedings. Paris, France: Space Propulsion Comitee/AAAF, 2014. p. 1-7. ISBN: 978-85-86686-70-2.
  Detail | WWW

  SYMONOV, V.; POPELA, R.; HLINKA, J.; JEBACEK, I. Composite Wing Leading Edge Design: Technical Specification. 2014. p. 1-13.
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  PEJCHAR, J.; DANIEL, M.; POPELA, R. SOFT LANDING TEST OF AN INTERPLANETARY PROBE IN THE EARTH CONDITIONS. In Sborník příspěvků Mezinárodní Masarykovy konference pro doktorandy a mladé vědecké pracovníky 2014. Hradec králové: MAGNANIMITA. 5. vyd. 2014. ISBN 978-80-87952-07-8, ETTN 042-14-14030-12- 4. 2014. Hradec Kralové: MAGNANIMITAS, 2014. p. 1-10. ISBN: 978-80-87952-07- 8.
  Detail | WWW

• 2013

  ZIKMUND, P.; POPELA, R. Wake vortex gliding as a new propulsion concept for UAVs. Letecký zpravodaj, 2013, vol. 2013, no. 2, p. 14-16. ISSN: 1211- 877X.
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• 2010

  HRADIL, J.; POPELA, R. Simplified CFD model of Synthetic Jet Actuator (SJA). Letecký zpravodaj, 2010, vol. 2010, no. 1, p. 48-50. ISSN: 1211- 877X.
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  POPELA, R.; DOUPNÍK, P. Response Surface Method Application to Transonic Business- jet Wing Optimization. Letecký zpravodaj, 2010, vol. 2010, no. 1, p. 23-27. ISSN: 1211- 877X.
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• 2009

  DRAHANSKÝ, M.; POPELA, R.; MARVAN, A.; ZIKMUND, P.; HOLENDA, S. SEDAQ - Ústředna pro sběr dat ze senzorů v UAV. Sborník příspěvků 9. mezinárodní vědecké konference MDS-PSL 2009. Brno: Univerzita Obrany, 2009. p. 28-31. ISBN: 978-80-7231-670-0.
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  DRAHANSKÝ, M.; MARVAN, A.; HOLENDA, S.; POPELA, R. Flight Data Wireless Digital Acquisition System. Letecký zpravodaj, 2009, vol. 2008, no. 2, p. 15-17. ISSN: 1211- 877X.
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• 2008

  DRAHANSKÝ, M.; MARVAN, A.; POPELA, R.; HOLENDA, S. Flight Data Wireless Digital Acquisition System. Proceedings of the RRDPAE2008. RESEARCH BULLETIN. Brno: Brno University of Technology, 2008. p. 1-5. ISSN: 1425-2104.
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• 2007

  PÍŠTĚK, A.; POPELA, R. The VUT 100/200 general aviation aircraft family: project and realization. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G- JOURNAL OF AEROSPACE ENGINEERING, 2007, vol. 2007, no. Vol 221 No G2, p. 193-197. ISSN: 0954- 4100.
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  POPELA, R.; ZIKMUND, P.; VANĚK, F.; KOUŘIL, M. The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft. Letecký zpravodaj, 2007, vol. 2007, no. 3, p. 52-55. ISSN: 1211- 877X.
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• 2004

  POPELA, R., HRNČÍŘ, Z. Experimental nad Numerical Study of Spanwise Fences. Letecký zpravodaj, 2004, vol. 2004, no. 2, p. 13-17. ISSN: 1211- 877X.
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• 2003

  POPELA, R. Rozbor zatížení VE SBH 20. Brno: MŠMT, 2003.
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  POPELA, R., HRNČÍŘ, Z. Ice Acreation Effect on Performance Degradation of MS(1)- 0313 Airfoil with Aileron. Letecký zpravodaj, 2003, vol. 2003, no. 3, ISSN: 1211- 877X.
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• 2002

  POPELA, R. Výpočetní ověření experimentální vysokovztlakové konfigurace Část I. 2002.
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  POPELA, R. Návrh vztlakové klapky letounu VUT 300 Zlín. 2002.
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• 2000

  POPELA, R. Numerické řešení 3D proudění komplexní konfigurace malého dopravního letounu. Letecký zpravodaj, 2000, vol. 2, no. 12, p. 6 ( p.)ISSN: 1211- 877X.
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