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Research Output 2009 2019

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Conference contribution
2018

Closed loop position and pre-stress control for a morphing aircraft wing with distributed multi-axis pneumatic actuation

Zhou, H., Plummer, A. & Cleaver, D., 14 Sep 2018, BATH/ASME 2018 Symposium on Fluid Power and Motion Control, FPMC 2018. American Society of Mechanical Engineers (ASME), p. V001T01A031 7 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Volumetric Velocimetry Measurements of Film Cooling Jets

Carvalho Batista Soares De Figueiredo, A. J., Jones, R., Pountney, O., Scobie, J., Lock, G., Sangan, C. & Cleaver, D., 11 Jun 2018, Proceedings of the ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers (ASME), 15 p. GT2018-75411

Research output: Chapter in Book/Report/Conference proceedingConference contribution

film cooling
kidneys
vortices
turbomachinery
momentum
2017

Experimental validation of tow-steered composite wings for aeroelastic design

Stodieck, O., Francois, G., Heathcote, D., Zympeloudis, E., Kim, B. C., Rhead, A. T., Cleaver, D. & Cooper, J. E., 1 Jan 2017, 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. International Forum on Aeroelasticity and Structural Dynamics (IFASD), Vol. 2017-June.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Frequency Response of Aerodynamic Load Control through Mini-tabs

Heathcote, D., Gursul, I. & Cleaver, D., 11 Jan 2017, 55th AIAA Aerospace Sciences Meeting, 2017. American Institute of Aeronautics and Astronautics, AIAA 2017-0947

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Aerodynamic loads
Frequency response
Aerodynamics
Force measurement
Airfoils
2015

Fluid-structure interactions for flexible and rigid tandem-wings at low Reynolds numbers

Jones, R., Cleaver, D. & Gursul, I., 2015, 53rd AIAA Aerospace Sciences Meeting: AIAA SciTech. American Institute of Aeronautics and Astronautics

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluid structure interaction
Reynolds number
Rigid wings
Flexible wings
Angle of attack