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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
1272009
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
1272009
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), 2011
1162011
Active control of separation on a wing with oscillating camber
D Munday, J Jacob
Journal of aircraft 39 (1), 187-189, 2002
1002002
Active control of separation on a wing with conformal camber
D Munday, J Jacob
39th Aerospace Sciences Meeting and Exhibit, 293, 2001
662001
Experimental comparison of axial turbine performance under steady and pulsating flows
AS George, R Driscoll, E Gutmark, D Munday
Journal of Turbomachinery 136 (11), 111005, 2014
62*2014
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
602015
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
572012
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
542015
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
422015
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
342002
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
302008
Flow structure of supersonic jets from conical CD nozzles
D Munday, E Gutmark, J Liu, K Kailasanath
39th AIAA fluid dynamics conference, 4005, 2009
272009
Supersonic jet noise reduction technologies for gas turbine engines
D Munday, N Heeb, E Gutmark, J Liu, K Kailasanath
262011
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
252013
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
Dependence of film cooling effectiveness on three-dimensional printed cooling holes
P Aghasi, E Gutmark, D Munday
Journal of Heat Transfer 139 (10), 102003, 2017
21*2017
Effect of the initial turbulence level on an underexpanded supersonic jet
J Liu, K Kailasanath, JP Boris, N Heeb, D Munday, E Gutmark
AIAA journal 51 (3), 741-745, 2013
162013
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
162012
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
162009
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