Dr.ir. B.W. van Oudheusden

profile

Biography

Dr. Bas van Oudheusden is associate professor in Aerodynamics at Delft University of Technology. He obtained his MSc degree at the Aerospace Engineering department of TU Delft in 1985 and his PhD in 1989 at the Electronics Engineering department of TU Delft, on the topic of a semi-conductor flow sensor. His current research interests are viscous flow effects at low and high speed regimes, shock wave – boundary layer interactions (SWBLI), unsteady flows (including flapping-wing aerodynamics) and “pressure-from-PIV”. Regarding the latter topic he published a review article in Measurement Science and Technology (2013, doi:10.1088/0957-0233/24/3/032001) and acted as co-ordinator of the EU-funded collaborative project NIOPLEX (2013-2016) and WP leader in its follow-up HOMER (2018-2020). He was also involved in two European projects on SWBLI: UFAST (2005-2009) and TFAST (2012-2016). He is (co-)author of approximately 160 scientific articles (Scopus, July 2018).

Projects

• Investigator and WP Leader in EU-H2020 project “HOMER” Holistic Optical Metrology for Aero-Elastic Research (2018-2021); total EU project budget M€ 4.91 
• Co-ordinator of EU-FP7 project “NIOPLEX” Non-intrusive optical pressure and loads extraction (2013-2016); total EU project budget M€ 1.68 
• Investigator in EU-FP7 project “TFAST” Transition efects of turbulent shock-wave boundary layer interactions (2012-2016)
• Investigator in EU-FP6 project “UFAST”: Unsteady Effects of turbulent shock-wave boundary layer interactions (2005-2009)
• Principal Investigator of STW-OTP project 11023 “Insect flight inspired new generation of flapping-wing Micro-Aircraft” (2010-2015)
• Principal Investigator of STW-OTP project  07645 “PIV-based non-intrusive determination of unsteady aerodynamic loads” (2007-2011)
• Co-Investigator of NWO-ALW project 814.02.019 “Optimal Aerodynamic Strategies in Insect Flight” (2005-2009)
• Co-Investigator of NWO-TTW projects15039 "A bio-inspired sensory-motor system for gust control of Micro Air Vehicles" (2017-2021)

subjects

2006 - Aerodynamics B

• Code: AE2110 ECTS Points: 3

2006 - Boundary Layer Flows - B

• Code: AE4171 ECTS Points: 3

2006 - Boundary Layer Flows - A

• Code: AE4170 ECTS Points: 3

2007 - Aerodynamics B

• Code: AE2110 ECTS Points: 3

2007 - Boundary Layer Flows - A

• Code: AE4170 ECTS Points: 3

2007 - Boundary Layer Flows - B

• Code: AE4171 ECTS Points: 3

2008 - Boundary Layer Flows - A

• Code: AE4170 ECTS Points: 3

2008 - Boundary Layer Flows - B

• Code: AE4171 ECTS Points: 3

2009 - Aerodynamics B

• Code: AE2110 ECTS Points: 3

2008 - Aerodynamics B

• Code: AE2110 ECTS Points: 3

2010 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2011 - Aerodynamics I

• Code: AE2102 ECTS Points: 3

2011 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2009 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2010 - Aerodynamics B

• Code: AE2110 ECTS Points: 3

2010 - Aerodynamics I

• Code: AE2102 ECTS Points: 3

2014 - Aerodynamics I

• Code: AE2130-I ECTS Points: 3

2014 - Aerodynamics Sub- and Supersonic

• Code: AE2130 ECTS Points: 7

2014 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2013 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2012 - Aerodynamics I

• Code: AE2102 ECTS Points: 3

2012 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2015 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2015 - Aerodynamics I

• Code: AE2130-I ECTS Points: 3

2015 - Aerodynamics Sub- and Supersonic

• Code: AE2130 ECTS Points: 7

2013 - Aerodynamics Sub- and Supersonic

• Code: AE2130 ECTS Points: 7

2013 - Aerodynamics I

• Code: AE2130-I ECTS Points: 3

2017 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2016 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2018 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2016 - Aerodynamics Sub- and Supersonic

• Code: AE2130 ECTS Points: 7

2019 - Viscous Flows

• Code: AE4120 ECTS Points: 3

2018 - Viscous Flows

• Code: AE4120 ECTS Points: 3

ancillary activities

No secondary work -

2018-01-01 - 2020-01-01