Mohd Yousuf Ali
Mohd Yousuf Ali
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SparkJet characterizations in quiescent and supersonic flowfields
T Emerick, MY Ali, C Foster, FS Alvi, S Popkin
Experiments in Fluids 55, 1-21, 2014
Dynamic Mode Decomposition of Fast Pressure Sensitive Paint Data
MY Ali, A Pandey, JW Gregory
Sensors 16 (6), 862, 2016
Jet arrays in supersonic crossflow - An experimental study
MY Ali, F Alvi
Physics of Fluids 27 (126102), 2015
Studies on the influence of steady microactuators on shock-wave/boundary-layer interaction
MY Ali, FS Alvi, R Kumar, C Manisankar, SB Verma, L Venkatakrishnan
AIAA journal 51 (12), 2753-2762, 2013
DMD and POD of time-resolved schlieren on a multi-stream single expansion ramp nozzle
MG Berry, MY Ali, AS Magstadt, MN Glauser
International Journal of Heat and Fluid Flow 66, 60-69, 2017
Spatially resolved mean and unsteady surface pressure in swept SBLI using PSP
LJ Mears, A Baldwin, MY Ali, R Kumar, FS Alvi
Experiments in Fluids 61 (4), 92, 2020
Low-dimensional and data fusion techniques applied to a supersonic multistream single expansion ramp nozzle
MNG Matthew G. Berry, Cory M. Stack, Andrew S. Magstadt, Mohd Y. Ali, Datta ...
Physical Review Fluids 2 (10), 100504, 2017
Flowfield of a 3-D swept shock boundary layer interaction in a Mach 2 flow
N Arora, MY Ali, FS Alvi
46th AIAA fluid dynamics conference, 3649, 2016
Generation and control of oblique shocks using microjets
R Kumar, MY Ali, FS Alvi, L Venkatakrishnan
AIAA journal 49 (12), 2751-2759, 2011
Flowfield measurements in a Mach 2 fin-generated shock/boundary-layer interaction
N Arora, MY Ali, Y Zhang, FS Alvi
AIAA Journal 56 (10), 3963-3974, 2018
Control of Resonant Flow Inside a Supersonic Cavity Using High Bandwidth Micro-Actuators
M Ali, J Solomon, J Gustavsson, R Kumar, F Alvi
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010
SparkJet actuator characterization in supersonic crossflow
T Emerick, M Ali, C Foster, F Alvi, S Haack Popkin, B Cybyk
6th AIAA Flow Control Conference, 2814, 2012
Cimetidine potentiation of warfarin action.
B Kerley, M Ali
Canadian Medical Association Journal 126 (2), 116, 1982
Studies on the control of shock wave-boundary layer interaction using steady microactuators
MY Ali, F Alvi, C Manisankar, S Verma, L Venkatakrishnan
41st AIAA Fluid Dynamics Conference and Exhibit, 3425, 2011
Shock-boundary layer interaction due to a sharp unswept fin in a Mach 2 flow
N Arora, MY Ali, Y Zhang, FS Alvi
53rd AIAA aerospace sciences meeting, 1517, 2015
Flowfield characteristics of oblique shocks generated using microjet arrays
M Ali, K Ahmed, R Kumar, F Alvi
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011
Velocity field measurements on high‐frequency, supersonic microactuators
PA Kreth, MY Ali, EJ Fernandez, FS Alvi
Experiments in Fluids 57 (5), 1-13, 2016
Mixing Characteristics of Active Microjet-Based Actuators in a Supersonic Backward-Facing Step Flow
K Ahmed, MY Ali, F Alvi
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011
Virtual shock shaping using microjet arrays
R Kumar, A Botu, MY Ali, FS Alvi, L Venkatakrishnan
AIAA paper 103, 2010, 2010
Properties of resonance enhanced microjets in supersonic crossflow
MY Ali, N Arora, M Topolski, FS Alvi, JT Solomon
AIAA Journal 55 (3), 1075-1081, 2017
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