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Oliver D. Wong
Observed names:
O. D. Wong,
O. Wong,
Oliver Wong,
Oliver. D. Wong
Observed institutions:
United States Department of the Army,
Georgia Institute of Technology,
Langley Research Center,
United States Army Combat Capabilities Development Command,
United States Army
OpenAlex ID:
A5049073748
Performance analysis of a wing with multiple winglets
2001
·
M. Smith
, N. Komerath
, et al.
·
AIAA Applied Aerodynamics Conference
·
100
Photogrammetric Measurements of an EH-60L Brownout Cloud
2010
·
Oliver D. Wong
, Philip E. Tanner
·
Journal of the American Helicopter Society
·
30
PDF
Blade Tip Pressure Measurements Using Pressure Sensitive Paint
2012
·
Oliver D. Wong
, A. Neal Watkins
, et al.
·
Journal of the American Helicopter Society
·
27
PDF
Pressure Sensitive Paint Measurements on 15% Scale Rotor Blades in Hover
2005
·
Oliver Wong
, A. Watkins
, et al.
·
AIAA Fluid Dynamics Conference and Exhibit
·
25
Development of a Pressure Sensitive Paint System for Measuring Global Surface Pressures on Rotorcraft Blades
2007
·
A. Neal Watkins
, Bradley D. Leighty
, et al.
·
International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF)
·
17
Deployment of a Pressure Sensitive Paint System for Measuring Global Surface Pressures on Rotorcraft Blades in Simulated Forward Flight
2012
·
Neal Watkins
, Bradley Leighty
, et al.
·
AIAA Aerodynamic Measurement Technology and Ground Testing Conference
·
13
PDF
Formation and evolution of tip vortices of an isolated rotor in forward flight
2001
·
Oliver D. Wong
·
UPT. Syiah Kuala University Library (Syiah Kuala University)
·
13
PDF
On the Formation and Decay of Rotor Blade Tip Vortices
2004
·
Narayanan Komerath
, Balakrishnan Ganesh
, et al.
·
AIAA Fluid Dynamics Conference and Exhibit
·
11
Experiments on the origin of tip-vortices
2000
·
Raghav Mahalingam
, Oliver Wong
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
·
10
Experimental Investigation of Active Aerodynamic Load Reduction on a Rotorcraft Fuselage with Rotor Effects
2014
·
Norman W. Schaeffler
, Brian G. Allan
, et al.
·
AIAA Applied Aerodynamics Conference
·
6
Development of a Large Field-of-View PIV System for Rotorcraft Testing in the 14- x 22-Foot Subsonic Tunnel
2009
·
Luther Jenkins
, Chung-Sheng Yao
, et al.
·
Vertical Flight Society Forum
·
5
Navier-Stokes Simulation of a Heavy Lift Slowed-Rotor Compound Helicopter Configuration
2009
·
Brian Allan
, Luther Jenkins
, et al.
·
Vertical Flight Society Forum
·
5
Aerodynamic Characteristics of Two Rotary Wing Uav Designs
2013
·
Henry E. Jones
, Oliver D. Wong
, et al.
·
NASA Technical Reports Server (NASA)
·
3
Initial Assessment of Surface Pressure Characteristics of two Rotary Wing UAV Designs
2006
·
Henry E. Jones
, Brendon D. Malovrh
, et al.
·
Vertical Flight Society Forum
·
1
Tip Vortex Formation and Evolution to the Near Wake of a Rotor in Forward Flight
2001
·
Oliver D. Wong
, Narayanan Komerath
·
Vertical Flight Society Forum
·
1
Mechanisms of Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects
2016
·
Norman Schaeffler
, Brian Allan
, et al.
·
NASA Technical Reports Server (NASA)
Active Aerodynamic Load Reduction on a Rotorcraft Fuselage with Rotor Effects - A CFD Validation Effort
2015
·
Brian Allan
, Oliver Wong
, et al.
·
Vertical Flight Society Forum
PDF
Deployment of a Pressure Sensitive Paint System for Measuring Global Surface Pressures on Rotorcraft Blades in Simulated Forward Flight: Preliminary PSP Results from Test 581 in the 14- by 22-Foot Subsonic Tunnel
2011
·
A. Neal Watkins
, Bradley D. Leighty
, et al.
·
NASA Technical Reports Server (NASA)
Tip Vortex Formation and Evolution to the Near Wake of a Rotor in Forward Flight
2001
·
Narayanan M. Komerath
, Oliver D. Wong
·
Vertical Flight Society Forum
Tunable Solid-State Laser and High Resolution Digital Cameras for Lagrangian Vortex Imaging
2000
·
N. M. Komerath
, O. D. Wong
, et al.
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Works count:
20
Citation count:
267
H-index:
9
I10-index:
9
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