Prof. Dr. Michel Guillaume
Prof. Dr. Michel Guillaume
ZHAW
School of Engineering
Technikumstrasse 9
8400 Winterthur
Persönliches Profil
Tätigkeit an der ZHAW als
Zentrumsleiter Zentrum für Aviatik
Dozent für die Fächer Aerodynamik und Strukturintegrität
Weitere Lehrtätigkeiten
ETHZ: Dozent für Betriebsfestigkeit am MAVT
CFAC-HSG: Aviation Management Course: Project Management in Aerospace
Rzeszow University of Technology (Poland): Structural Integrity Short Course (Gastdozent)
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)
Projekte
Projektleitung
- Zivile Drohnen Studie für TA-SWISS / / 01.06.2016
- Sicherstellung der Strukturintegrität, Damage Tolerance-Analysen von Ageing Aircrafts / / 01.01.2016
- CleanLE2: Demonstration of a Decontamination Device Prototype for Business Jets and Experimental Validation / / 25.06.2014
Publikationen
Beiträge, peer-reviewed
; ; ; (2016).
Aerostructural Performance of Distributed Compliance Morphing Wings: Wind Tunnel and Flight Testing
.
AIAA Journal, 54, 12. 3859 - 3871. Peer reviewed.
; ; ; ; (2015).
Design and experimental characterisation of a morphing wing with enhanced corrugated skin
.
Intelligent Material Systems and Structures / SAGE, 1-15, DOI: 10.1177/1045389X15595296. Peer reviewed.
; (2015).
Structural Analysis of Ageing Pilatus P-3 Engine Mount
.
Porcedia Engineering; 1877-7058, 2015 Punlished by Elesevier Ltd, 114 583-589. Peer reviewed.
; ; ; (2014).
Structural Integrity - Yesterday - Today - Tomorrow
.
Advanced Materials Research / Trans Tech Publications, Switzerland, 891 - 892, AMR.891-892.1053. 1053 - 1058. Peer reviewed.
(2014).
Structural Integrity for Aging Airplanes
.
In: ICAS International Conference 2014 in St. Petersbourg (ISBN: 3-932182-80-4). St. Petersbourg: Deutsche Gesellschaft für Luft und Raumfahrt, Bonn (D). Peer reviewed.
Beiträge, nicht peer-reviewed
(2016).
Future Aircraft Technologies
.
In: SR Technics Workshop Event Technikerschule. Winterthur: FTS SRT.
(2016).
What does the future hold for unmanned aircraft systems ?
: Gold Rush or Reality ?.
In: swissnex Boston Event, Keynote and Panel Discussion. Boston: swissnex.
(2015).
Ermittlung von Materialermüdung: Simulation oder Tests
.
In: VPE Swiss Workshop am 18. Juni 2015, HSR Rapperswil. Rapperswil: HSR.
; Manfriani, Leonardo (2015).
Low Speed Wind Tunnel at ZHAW
.
In: 51th Annual Meeting Subsonic Aerodynamic Testing Association. Newport News: NASA.
(2015).
Review of Aeronautical Fatigue Investigations in Switzerland April 2013 - March 2015
.
In: ICAF 2015 Structural Integrity: Embracing the future - respecting the past; supporting aging fleets with new technologies; ISBN 978-951-387442-1. Proceedings of the 35th Conference and the 28th Symposium of the International Fatigue and Structural Integrity, 1 - 5 June, Helsinki, Finland. Helsinki: VTT Technical Research Center of Finland Ltd.
(2015).
Wie kann ein Flugzeug fliegen ?
: Interdisziplinär: Kinder fragen Experten.
aktuelletechnik.ch, 2. 16-17.
(2014).
Innovation in Aviation (Centre for Aviation)
.
TransNetAero Meeting in Altenrhein St. Gallen 25.03.2014
; (2014).
New Wind Tunnel at ZHAW
.
50th Subsonic Aerodynamic Testing Association (SATA) held by Airbus in Bremen June 2014
(2013).
33rd ICAF Conference June 2013
: Review of Aeronautical Fatigue Investigations in Switzerland (2011 - 2013).
In: . Jerusalem: Paragon Group.
(2013).
Interdisziplinäre Forschung und Entwicklung in der Aviatik; AERO 2013 Friederichshafen
.
In: . Friederichshafen: AERO.
(2013).
Structural Integrity - Yesterday - Today - Tomorrow
.
In: Massachusetts Institute of Technology (MIT) AeroAstra Seminar 09.10.2013; . Massachusetts: MIT.
; (0).
Structural Analysis of Ageing Pilatus P-3 Engine Mount
.
Porcedia Engineering; 1877-7058, 2015 Punlished by Elesevier Lt
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