Matthew J. Ringuette
Matthew J. Ringuette
University at Buffalo, The State University of New York, Department of Mechanical & Aerospace
Verified email at - Homepage
Cited by
Cited by
Role of the tip vortex in the force generation of low-aspect-ratio normal flat plates
MJ Ringuette, M Milano, M Gharib
Journal of Fluid Mechanics 581, 453-468, 2007
Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3
MJ Ringuette, M Wu, MP Martin
Journal of fluid Mechanics 594, 59-69, 2008
Finite-span rotating wings: three-dimensional vortex formation and variations with aspect ratio
ZR Carr, C Chen, MJ Ringuette
Experiments in fluids 54 (2), 1-26, 2013
Aspect-ratio effects on rotating wings: circulation and forces
ZR Carr, AC DeVoria, MJ Ringuette
Journal of Fluid Mechanics 767, 497-525, 2015
Vortex formation and saturation for low-aspect-ratio rotating flat-plate fins
AC DeVoria, MJ Ringuette
Experiments in fluids 52 (2), 441-462, 2012
Experimental study of a Mach 3 compression ramp interaction at Re {theta}= 2400
MJ Ringuette, P Bookey, C Wyckham, AJ Smits
AIAA journal 47 (2), 373-385, 2009
Low Reynolds number effects in a Mach 3 shock/turbulent-boundary-layer interaction
M Ringuette, M Wu, MP Martin
AIAA journal 46 (7), 1883-1886, 2008
On calculating forces from the flow field with application to experimental volume data
AC DeVoria, ZR Carr, MJ Ringuette
Journal of fluid mechanics 749, 297-319, 2014
The effect of aspect ratio on the three-dimensional vortex formation of rotating flat-plate wings
Z Carr, C Chen, M Ringuette
50th AIAA aerospace sciences meeting including the new horizons forum and …, 2012
Vortex formation and saturation for low-aspect-ratio rotating flat plates at low Reynolds number
A DeVoria, P Mahajan, M Ringuette
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011
Vortex formation and drag on low aspect ratio, normal flat plates
MJ Ringuette
California Institute of Technology, 2004
The turbulence structure of shockwave and boundary layer interactions in a compression corner
A Smits, MP Martin, M Wu, M Ringuette
44th AIAA Aerospace Sciences Meeting and Exhibit, 497, 2006
Leading edge vortex evolution and lift production on rotating wings
AR Jones, F Manar, N Phillips, T Nakata, R Bomphrey, MJ Ringuette, ...
54th AIAA Aerospace Sciences Meeting, 0288, 2016
Characterization of the turbulence structure in supersonic boundary layers using DNS data
M Ringuette, MP Martin, A Smits, M Wu
36th AIAA Fluid Dynamics Conference and Exhibit, 3539, 2006
The Flow Structure of Low-Aspect-Ratio Rotating Wings from Dye Visualization
ZR Carr, MJ Ringuette
AIAA Journal 52 (5), 1081-1086, 2014
Experimental investigation of hypersonic turbulent boundary layer
D Sahoo, M Ringuette, A Smits
47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2009
Wall-Pressure Measurements in a Mach 3 Shock-Wave Turbulent Boundary Layer Interaction at a DNS Accessible Reynolds Number
M Ringuette, A Smits
37th AIAA Fluid Dynamics Conference and Exhibit, 4113, 2007
On the flow generated on the leeward face of a rotating flat plate
AC DeVoria, MJ Ringuette
Experiments in fluids 54 (4), 1-14, 2013
The vortex formation of an unsteady translating plate with a rotating tip
J Chowdhury, L Cook, MJ Ringuette
AIAA Scitech 2019 Forum, 0348, 2019
The force and impulse of a flapping plate performing advancing and returning strokes in a quiescent fluid
AC DeVoria, MJ Ringuette
Experiments in fluids 54 (5), 1-15, 2013
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