Author

David Riordan

Observed names: D Riordan, D. Riordan, Riordan, D, Riordan, D., Riordan, David 1960-

Observed institutions: Queen's University Belfast, Bombardier (United Kingdom), Bombardier (Canada)

OpenAlex ID: A5069614421

Implementation of Menter's Transition Model on an Isolated Natural Laminar Flow Nacelle

2011 · Yujing Lin, Theresa Robinson, et al. · AIAA Journal · 31

Key aerodynamic technologies for aircraft engine nacelles

2006 · S. Raghunathan, E. Benard, et al. · The Aeronautical Journal · 20

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Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons

2009 · B Sloan, J Wang, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 8

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Theory and Practice of Aircraft Performance

2016 · Ajoy Kumar Kundu, David Riordan, et al. · CERN Document Server (European Organization for Nuclear Research) · 7

Methodologies for Structural Optimisation of a Thrust Reverser Cascade Using a Multidisciplinary Approach

2003 · Joe Butterfield, H. Yao, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 6

Numerical Simulation on Flow Fields of the Nature Blockage Thrust Reverser

2005 · Hui Yao, Srinivasan Raghunathan, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 5

The Effect of the Porous Diverter Fairing on the Aerodynamic Performance of Natural Blockage Thrust Reverser

2004 · Hui Yao, Richard Cooper, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 4

Investigations on Variable Fan Nozzle Area to Reduce the Aircraft Jet Noise

2007 · Hui Yao, John Richardson, et al. · 7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero Sciences,17th LTA Systems Tech Conf; followed by 2nd TEOS Forum · 3

Influence of Surface Waviness for Laminar Flow Nacelle Applications

2009 · Humberto Medina, Juliana Early, et al. · AIAA Applied Aerodynamics Conference · 2

Investigation of fire propagation within zone one of an engine nacelle

1999 · K. Donaghy, D. Riordan, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 2

The effect of a wall normal vibration on a turbulent boundary layer

2002 · C. Regan, E. Benard, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 1

Identification of aircraft noise at landing

2005 · Jian Wang, Hui Yao, et al. · AIAA/CEAS Aeroacoustics Conference

Methodologies for Structural Optimisation of a Thrust Reverser Cascade Using Aerodynamic and Structural Integration

2003 · Joseph Butterfield, Hui Yao, et al. · Research Portal (Queen's University Belfast)

Excrescence effects on boundary layers with pressure gradient at high subsonic speeds

2002 · S. Raghunathan, D. Riordan, et al. · AIAA Aerospace Sciences Meeting and Exhibit

Works count: 19

Citation count: 92

H-index: 5

I10-index: 2