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Wing Ng
Wing Ng
Verified email at vt.edu
Title
Cited by
Cited by
Year
Improving control system effectiveness for ducted fan VTOL UAVs operating in crosswinds
J Fleming, T Jones, W Ng, P Gelhausen, D Enns
2nd AIAA" Unmanned Unlimited" Conf. and Workshop & Exhibit, 6514, 2003
1292003
Improving ducted fan UAV aerodynamics in forward flight
W Graf, J Fleming, W Ng
46th AIAA aerospace sciences meeting and exhibit, 430, 2008
812008
Effects of large scale high freestream turbulence and exit reynolds number on turbine vane heat transfer in a transonic cascade
S Nasir, JS Carullo, WF Ng, KA Thole, H Wu, LJ Zhang, HK Moon
802009
High‐frequency temperature and pressure probe for unsteady compressible flows
WF Ng, AH Epstein
Review of Scientific Instruments 54 (12), 1678-1683, 1983
731983
Numerical investigation of tandem airfoils for subsonic axial-flow compressor blades
J McGlumphy, WF Ng, SR Wellborn, S Kempf
712009
Preconditioned conjugate gradient methods for the Navier-Stokes equations
K Ajmani, WF Ng, MS Liou
Journal of Computational Physics 110 (1), 68-81, 1994
691994
Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade: Part II—Unsteady Heat Transfer
O Popp, DE Smith, JV Bubb, HC Grabowski III, TE Diller, JA Schetz, ...
Turbo Expo: Power for Land, Sea, and Air 78569, V003T01A011, 2000
672000
Experimental measurements and modeling of the effects of large-scale freestream turbulence on heat transfer
AC Nix, TE Diller, WF Ng
642007
3D numerical investigation of tandem airfoils for a core compressor rotor
J McGlumphy, WF Ng, SR Wellborn, S Kempf
632010
Reduction of unsteady stator–rotor interaction using trailing edge blowing
TA Leitch, CA Saunders, WF Ng
Journal of sound and vibration 235 (2), 235-245, 2000
622000
A novel transient technique to determine recovery temperature, heat transfer coefficient, and film cooling effectiveness simultaneously in a transonic turbine cascade
S Xue, A Roy, WF Ng, SV Ekkad
Journal of Thermal Science and Engineering Applications 7 (1), 2015
612015
Wind tunnel aeroacoustic measurements of a 26%-scale 777 main landing gear
P Ravetta, R Burdisso, W Ng
10th AIAA/CEAS Aeroacoustics Conference, 2885, 2004
602004
Aerodynamic performance of a high-turning compressor stator with flow control
C Carter, S Guillot, W Ng, W Copenhaver
37th Joint propulsion conference and exhibit, 3973, 2001
562001
The effects of freestream turbulence, turbulence length scale, and exit Reynolds number on turbine blade heat transfer in a transonic cascade
JS Carullo, S Nasir, RD Cress, WF Ng, KA Thole, LJ Zhang, HK Moon
552011
Unsteady losses in transonic compressors
WF Ng, AH Epstein
541985
High intensity, large length-scale freestream turbulence generation in a transonic turbine cascade
AC Nix, AC Smith, TE Diller, WF Ng, KA Thole
Turbo Expo: Power for Land, Sea, and Air 36088, 961-968, 2002
532002
Experimental demonstration of active flow control to reduce unsteady stator-rotor interaction
NM Rao, J Feng, RA Burdisso, WF Ng
AIAA journal 39 (3), 458-464, 2001
492001
Development and application of a point Doppler velocimeter featuring two-beam multiplexing for time-resolved measurements of high-speed flow
T Ecker, DR Brooks, KT Lowe, WF Ng
Experiments in fluids 55 (9), 1-15, 2014
462014
Aerodynamic/aeroacoustic testing in anechoic closed test sections of low-speed wind tunnels
T Ito, H Ura, K Nakakita, Y Yokokawa, W Ng, R Burdisso, A Iwasaki, ...
16th AIAA/CEAS aeroacoustics conference, 3750, 2010
452010
Effect of loading level and distribution on LPT losses
C Prakash, DG Cherry, HW Shin, J Machnaim, L Dailey, R Beacock, ...
Turbo Expo: Power for Land, Sea, and Air 43161, 917-925, 2008
402008
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