Prof. Dr. Michel Guillaume

Tätigkeit an der ZHAW als

Zentrumsleiter Zentrum für Aviatik
Dozent für die Fächer Aerodynamik und Strukturintegrität, Unmanned Aviation

Weitere Lehrtätigkeiten
ETHZ: Dozent für Betriebsfestigkeit am MAVT
TEKO: Dozent für Aircraft Structural Design and Repair
CFAC-HSG: Aviation Management Course: Project Management in Aerospace
Rzeszow University of Technology (Poland): Structural Integrity Short Course (Gastdozent)

http://zav.zhaw.ch

Arbeits- und Forschungsschwerpunkte, Spezialkenntnisse

Unmanned Aircraft Systems

Aerodynamik & Flugmechanik, Windkanal

Materialermüdung, Betriebsfestigkeit, Strukturintegrität

Flugzeug Entwicklung

Projektmanagement in der Luftfahrtindustrie

Aus- und Fortbildung

1985 - 1990: Studium der Physik an der ETH Zürich; dipl. phys. ETHZ
1991 - 1994: Doktorat an der ETH Zürich zum Thema Neutronenstreuung an
Hochtemperatursupraleitern; Dr. sc. nat. ETHZ
1998 - 1999: Nachdiplomstudium Ganzheitliches Management NDS FH an der Fachhochschule
Nordwestschweiz

Beruflicher Werdegang

2004 - 2012: General Manager Aerodynamics Center bei RUAG Aviation

1999 - 2004: Projektleiter F/A-18 Full Scale Fatigue Test bei RUAG Aerospace

1994 - 1999: Fatigue Engineer im Ressort Engineering im Flugzeugwerk Emmen / RUAG Aerospace

Mitglied in Netzwerken

• Swiss Aerospace Cluster
• International Committee on Aeronautical Fatigue and Structural Integrity (ICAF)
• Schweizerische Vereinigung für Flugwissenschaften (svfw)
• American Institute of Aeronautics and Astronautics (AIAA)
• Schweizerische Physikalische Gesellschaft (SPS)

• Zivile Drohnen Studie für TA-SWISS Stiftung / ProjektleiterIn / 01.06.2016
• Sicherstellung der Strukturintegrität, Damage Tolerance-Analysen von Ageing Aircrafts / ProjektleiterIn / 01.01.2016
• CleanLE2: Demonstration of a Decontamination Device Prototype for Business Jets and Experimental Validation / ProjektleiterIn / 25.06.2014

• Molinari, Giulio; Arrieta, Andres F.; Guillaume, Michel; Ermanni, Paolo,

  2016.

  Aerostructural performance of distributed compliance morphing wings : wind tunnel and flight testing

  .

  AIAA Journal.

  54(12),

  S. 3859-3871.

  Verfügbar unter: https://doi.org/10.2514/1.J055073

• Guillaume, Michel,

  2016.

  Future aircraft technologies

  .

  In:

  SR Technics Workshop Event Technikerschule, Winterthur, 2016.

• Guillaume, Michel,

  2016.

  What does the future hold for unmanned aircraft systems? : gold rush or reality?

  .

  In:

  Gold rush or realities? The future of drone systems, swissnex Boston, Boston, 29 September 2016.

• Previtali, Francesco; Molinari, Giulio; Arrieta, Andres F.; Guillaume, Michel; Ermanni, Paolo,

  2015.

  Design and experimental characterisation of a morphing wing with enhanced corrugated skin

  .

  Journal of Intelligent Material Systems and Structures.

  27(2),

  S. 278-292.

  Verfügbar unter: https://doi.org/10.1177/1045389X15595296

• Guillaume, Michel; Schläpfer, Elias; Schmid, Marcel,

  2015.

  Structural analysis of ageing Pilatus P-3 engine mount

  .

  Procedia Engineering.

  114,

  S. 583-589.

  Verfügbar unter: https://doi.org/10.21256/zhaw-3915

• Guillaume, Michel,

  2015.

  Review of aeronautical fatigue investigations in Switzerland April 2013 - March 2015

  [Paper].

  In:

  Proceedings of the 35th Conference and the 28th Symposium of the International Fatigue and Structural Integrity, 1 - 5 June, Helsinki, Finland.

  34th Conference of the International Committee on Aeronautical Fatigue and Structural Integrity (ICAF) : Embracing the future - respecting the past; supporting aging fleets with new technologies, Helsinki, Finland, 1-2 June 2015.

  Helsinki:

  VTT Technical Research Center of Finland Ltd.

• Guillaume, Michel; Manfriani, Leonardo,

  2015.

  Low speed wind tunnel at ZHAW

  .

  In:

  51th annual SATA (Subsonic Aerodynamic Testing Association) meeting, Newport News, 2015.

• Guillaume, Michel,

  2015.

  Ermittlung von Materialermüdung : Simulation oder Tests

  .

  In:

  VPE Swiss Workshop, Hochschule für Technik Rapperswil, Rapperswil, 18. Juni 2015.

• Guillaume, Michel,

  2014.

  Structural integrity for aging airplanes

  [Paper].

  In:

  Proceedings / 29th Congress of the International Council of the Aeronautical Sciences : St. Petersburg, Russia, September 7 - 12, 2014.

  29th Congress of the International Council of the Aeronautical Sciences, St. Petersburg, Russia, September 7 - 12, 2014.

  Bonn:

  International Council of the Aeronautical Sciences.

  Verfügbar unter: https://doi.org/10.21256/zhaw-3916

• Guillaume, Michel; Uebersax, Andreas; Mandanis, Georges; Huber, Cyril,

  2014.

  Structural integrity : yesterday - today - tomorrow

  [Paper].

  In:

  11th International Fatigue Congress, Melbourne, 2-7 March 2014.

  Trans Tech Publications.

  1053-1058.

  Verfügbar unter: https://doi.org/10.4028/www.scientific.net/AMR.891-892.1053

• Guillaume, Michel; Riedberger, Michael,

  2014.

  New wind tunnel at ZHAW

  .

  In:

  50th annual SATA meeting, Bremen, June 2014.

• Guillaume, Michel,

  2014.

  Innovation in aviation

  .

  In:

  TransNetAero meeting, Altenrhein St. Gallen, 25. März 2014.

• Guillaume, Michel,

  2013.

  Structural integrity : yesterday - today - tomorrow

  .

• Guillaume, Michel,

  2013.

  Review of aeronautical fatigue investigations in Switzerland (2011 - 2013)

  .

  In:

  33rd ICAF Conference, Jerusalem, June 2013.

• Guillaume, Michel,

  2013.

  Interdisziplinäre Forschung und Entwicklung in der Aviatik

  .

  In:

  AERO 2013, Friederichshafen, 24-27 April 2013.

Publikationen vor Tätigkeit an der ZHAW

Swiss / Finnish Computational Fluid Dynamics Simulation on the F/A-18, Paper & Presentation at 28th International Congress of the Aeronautical Sciences (ICAS) 2012 in September 2012 (ICAS2012-10.6.1; ISBN 978-0-9565333-1-9)

Moderne Strömungssimulation für Flugzeuge; Schweizerische Vereinigung für Flugwissenschaften am 17. November 2011 an der ETH Zürich

F/A-18 Vertical tail Buffeting Calculation using unsteady Fluid Structure Interaction; The Aeronautical Journal, May 2011, Volume 115, No. 1166

The Challenge of large Composite Transport Airplanes during their Life Cycle; Paper and Keynote Presentation 5th International Conference on Composites Testing and Model Identification; ETH Lausanne Februar 2011

Windbreak? The F/A-18, and the HISAC Projects. His Ultimate Vision is using CFD for virtual Flight Testing; Interview in Aerospace Testing International, September 2009 p47-48

Calculation of Unsteady Loads for the F/A-18 Vertical Tail Buffeting; Paper and Presentation 1st CEAS European Air and Space Conference in Berlin, September 2007

Latest development in RUAG Aerospace’s Wind Tunnels and Balance technology at RUAG Aerospace 43rd Meeting of Subsonic Aerodynamic Testing Association (SATA), June 2007

Calculations of F/A-18 Fatigue Loads and wing Deformation using Computational Fluid Dynamics; 25th International Congress of the Aeronautical Sciences (ICAS) 2006 in Hamburg

The Swiss F/A-18 Full Scale fatigue Test – Modern and Efficient Testing; ATIO AIAA Conference September 2004 in Chicago

Der F/A-18 – ein Flugzeug, das so nie fliegen darf; Paper & Präsentation Automotive Day; 12. November 2003 an der HTI Biel

Crack Initiation and Crack Growth Tests and Analysis at Center Hole Specimen for 7050-T7451, 7075-T7351;Ti-6Al-4V (RA); Paper & Presentation at 8th International Fatigue Congress 2002 in Stockholm

Swiss F/A-18 Full Scale Fatigue Test; Paper & Presentation at ICAF Conference 2001 in Toulouse, ICAF-Doc 2289

A residual Stress Model for Spectrum Crack Growth Analysis; International Journal of Fracture 1997, Vol 85, No. 2

Influence of Thickness on Crack Growth Life of Coldworked Holes; Paper & Presentation at ICAF 1997 in Edinburgh Scotland; ICAF-Doc 2177