Research

Heritage

Active flow control and fluid-structure interaction work supported by United States defence research agencies, alongside microprocessor thermo-mechanics work with academic and industrial partners.

• Active flow control for XV15 and V-22 Osprey tiltrotors — supported by DARPA
• Active flow control for Hurley wings — supported by the Air Force Office of Scientific Research
• Fluid-structure interaction for Hurley wings — supported by the Air Force Office of Scientific Research
• Active flow control and Coanda effect on cylinders — supported by the Office of Naval Research
• Active flow control on trucks — supported by Vinnova, Sweden
• Stress concentration methods for general geometries — supported by University of Arizona
• Thermo-mechanical stresses and J-integrals of microchips on laminated substrates — supported by University of Arizona and Intel Corporation