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Asad Asghar
Asad Asghar
Royal Military College, University of Notre Dame, KFUPM
Dirección de correo verificada de alumni.nd.edu
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Citado por
Citado por
Año
Velocity Characteristics of Turbulent Natural Convection in Symmetrically and Asymmetrically Heated Vertical Channels
MA Habib, SAM Said, SA Ahmed, A Asghar
Experimental Thermal and Fluid Science 26, 77-87, 2002
1042002
Heat Transfer Characteristics of Pulsated Turbulent Pipe Flow
MA Habib, SAM Said, A Asghar
Heat and Mass Transfer 34 (5), 413-421, 1999
551999
Experimental Investigations of the Vortex Flow on Delta Wings at High Incidence
WH Stahl, M Mahmood, A Asghar
AIAA Journal 30 (4), 1027-1032, 1992
511992
Phase synchronization of vortex shedding from multiple cylinders using plasma actuators
A Asghar, E Jumper
41st Aerospace Sciences Meeting and Exhibit, 1028, 2003
462003
Numerical investigation of the influence of real world blade profile variations on the aerodynamic performance of transonic nozzle guide vanes
R Edwards, A Asghar, R Woodason, M LaViolette, KG Boulama, ...
262012
Application of leading-edge tubercles to enhance propeller performance
A Asghar, RE Perez, PW Jansen, WDE Allan
AIAA Journal 58 (11), 4659-4671, 2020
232020
Performance evaluation of an S-duct diffuser of a flight-vehicle inlet in high-subsonic flow
A Asghar, RA Stowe, WDE Allan, D Alexander
Turbo Expo: Power for Land, Sea, and Air 56628, V001T01A027, 2015
192015
A preliminary study in regularizing the coherent structures in a planar, weakly-compressible, free shear layer
J Siegenthaler, A Asghar, E Jumper
41st Aerospace Sciences Meeting and Exhibit, 680, 2003
192003
Entrance aspect ratio effect on S-Duct inlet performance at high-subsonic flow
A Asghar, RA Stowe, WDE Allan, D Alexander
Journal of Engineering for Gas Turbines and Power 139 (5), 052602, 2017
182017
Phase synchronization of vortex shedding from two circular cylinders using plasma actuators
A Asghar, EJ Jumper
AIAA journal 47 (7), 1608-1616, 2009
182009
Experimental Evaluation of Service-Exposed Nozzle Guide Vane Damage in a Rolls Royce A-250 Gas Turbine
D Bouchard, A Asghar, M LaViolette, WDE Allan, R Woodason
Journal of Engineering for Gas Turbines and Power 136 (10), 102601, 2014
172014
Influence of a novel 3D leading edge geometry on the aerodynamic performance of low pressure turbine blade cascade vanes
A Asghar, WDE Allan, M LaViolette, R Woodason
Turbo Expo: Power for Land, Sea, and Air 45622, V02CT38A024, 2014
152014
Reynolds number effect of leading edge tubercles on airfoil aerodynamics
LH Peristy, RE Perez, A Asghar, WD Allan
34th AIAA Applied Aerodynamics Conference, 3260, 2016
142016
Assessment of the flow quality of a transonic turbine cascade
R Woodason, A Asghar, WDE Allan
Turbo Expo: Power for Land, Sea, and Air 48883, 1131-1141, 2009
142009
On the use of Reynolds Number as the Scaling Parameter for the Performance of Plasma Actuator in a Weakly Compressible Flow
A AsgharTP, EJ Jumper Jr, TC Corke
44th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2006
142006
Investigation of a passive flow control device in an s-duct inlet of a propulsion system with high subsonic flow
A Asghar, S Sidhu, WDE Allan, G Ingram, TM Hickling, R Stowe
Turbo Expo: Power for Land, Sea, and Air 50985, V001T01A033, 2018
102018
Turbulent Natural Convection in Vertical Short Channels
MA Habib, SAM Said, I Ahmed, SA, Ouwais, A Asghar
Turbulent Heat Transfer III conference, 2001
92001
Influence of a Novel Three-Dimensional Leading Edge Geometry on the Aerodynamic Performance of Transonic Cascade Vanes
D Bouchard, A Asghar, J Hardes, R Edwards, WDE Allan, M LaViolette
Turbo Expo: Power for Land, Sea, and Air 44748, 1597-1608, 2012
82012
S-Duct Diffuser Offset-to-Length Ratio Effect on Aerodynamic Performance of Propulsion-System Inlet of High Speed Aircraft
A Asghar, WDE Allan, M LaViolette, R Stowe, D Alexander, G Ingram
Turbo Expo: Power for Land, Sea, and Air 50985, V001T01A035, 2018
72018
Effects of combustion chamber geometry deviations upon exit temperature profiles for populations with varied service limitations
C Kotzer, M LaViolette, W Allan, A Asghar
72011
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
Artículos 1–20