David Munday
David Munday
Associate Professor, Miami University
Verified email at MiamiOH.edu
Title
Cited by
Cited by
Year
Large-eddy simulations of a supersonic jet and its near-field acoustic properties
J Liu, K Kailasanath, R Ramamurti, D Munday, E Gutmark, R Lohner
AIAA journal 47 (8), 1849-1865, 2009
1132009
Large-eddy simulations of a supersonic jet and its near-field acoustic properties
J Liu, K Kailasanath, R Ramamurti, D Munday, E Gutmark, R Lohner
AIAA journal 47 (8), 1849-1865, 2009
1132009
Flow structure and acoustics of supersonic jets from conical convergent-divergent nozzles
D Munday, E Gutmark, J Liu, K Kailasanath
Physics of Fluids 23 (11), 116102, 2011
852011
Active control of separation on a wing with oscillating camber
D Munday, J Jacob
Journal of aircraft 39 (1), 187-189, 2002
752002
Active control of separation on a wing with conformal camber
D Munday, J Jacob
39th Aerospace Sciences Meeting and Exhibit, 293, 2001
672001
Impact of deck and jet blast deflector on the flow and acoustic properties of an imperfectly expanded supersonic jet
J Liu, A Corrigan, K Kailasanath, R Ramamurti, N Heeb, D Munday, ...
Naval Engineers Journal 127 (3), 47-60, 2015
542015
Experimental comparison of axial turbine performance under steady and pulsating flows
AS George, R Driscoll, E Gutmark, D Munday
Journal of Turbomachinery 136 (11), 2014
502014
Development of a rotating detonation engine facility at the University of Cincinnati
AC St. George, RB Driscoll, DE Munday, EJ Gutmark
53rd AIAA Aerospace Sciences Meeting, 0635, 2015
392015
Experimental and numerical investigation ofaerodynamic flow control using oscillating adaptive surfaces
D Munday, J Jacob, T Hauser, G Huang
1st Flow Control Conference, 2837, 2002
302002
Acoustic effect of chevrons on supersonic jets exiting conical convergent-divergent nozzles
D Munday, N Heeb, E Gutmark, J Liu, K Kailasanath
AIAA journal 50 (11), 2336-2350, 2012
282012
Fuel blending as a means to achieve initiation in a rotating detonation engine
AC St. George, RB Driscoll, V Anand, DE Munday, EJ Gutmark
53rd AIAA aerospace sciences meeting, 0633, 2015
252015
Large-eddy simulations of a supersonic heated jet
J Liu, K Kailasanath, N Heeb, D Munday, E Gutmark
17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference …, 2011
242011
Flow structure of supersonic jets from conical cd nozzles
D Munday, E Gutmark, J Liu, K Kailasanath
39th AIAA Fluid Dynamics Conference, 4005, 2009
222009
Flow and acoustic radiation from realistic tactical jet CD nozzles
D Munday, E Gutmark, J Liu, K Kailasanath
14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference …, 2008
222008
Acoustic Effect of Chevrons on Jets Exiting Conical CD Nozzles
D Munday, N Heeb, E Gutmark, J Liu, K Kailasanath
15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference …, 2008
202008
Computational study of shock-associated noise characteristics using LES
J Liu, AT Corrigan, K Kailasanath, NS Heeb, DE Munday, EJ Gutmark
19th AIAA/CEAS Aeroacoustics Conference, 2199, 2013
192013
Supersonic jet noise reduction technologies for gas turbine engines
D Munday, N Heeb, E Gutmark, J Liu, K Kailasanath
Journal of engineering for gas turbines and power 133 (10), 2011
182011
Dependence of Film Cooling Effectiveness on Three-Dimensional Printed Cooling Holes
P Aghasi, E Gutmark, D Munday
Journal of Heat Transfer 139 (10), 2017
16*2017
Impact of mechanical chevrons on supersonic jet flow and noise
K Kailasanath, J Liu, E Gutmark, D Munday, S Martens
Turbo Expo: Power for Land, Sea, and Air 48821, 83-90, 2009
152009
Effect of nozzle-exit flow conditions on the flow and acoustic properties of imperfectly expanded supersonic jets
J Liu, K Kailasanath, J Boris, N Heeb, D Munday, E Gutmark
18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference …, 2012
142012
The system can't perform the operation now. Try again later.
Articles 1–20