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William Solomon
Observed names:
W Solomon,
W. David Solomon,
William D. Solomon
Observed institutions:
General Electric (United States),
Northrop Grumman (United States),
Ohio Aerospace Institute
OpenAlex ID:
A5087895980
Experimental Investigation of the Effects of a Moving Shock Wave on Compressor Stator Flow
2005
·
Matthew D. Langford
, Andrew Breeze-Stringfellow
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
·
13
Experimental Investigation of the Effects of a Moving Shock Wave on Compressor Stator Flow
2005
·
Matthew D. Langford
, Andrew Breeze-Stringfellow
, et al.
·
Journal of Turbomachinery
·
10
Flight Testing of a 30-Degree Sweep Laminar Flow Wing for a High-Altitude Long-Endurance Aircraft
2010
·
Aaron Drake
, William Solomon
·
AIAA Applied Aerodynamics Conference
·
9
The effects of blade count on boundary layer development in a low-pressure turbine
2000
·
Daniel Dorney
, Horia Flitan
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
·
8
Experiments and Analyses of Distributed Exhaust Nozzles
2005
·
Kevin W. Kinzie
, David B. Schein
, et al.
·
AIAA Journal
·
6
PDF
Large Jet-Noise Reductions Through Distributed Nozzles
2002
·
R Gaeta
, K Ahuja
, et al.
·
AIAA/CEAS Aeroacoustics Conference
·
6
Direct Numerical Simulation of Riblets Applied to Gas Turbine Compressor Blades at On- and Off-Design Incidences
2023
·
Melissa Kozul
, Massimiliano Nardini
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
·
5
Comparison of Boundary Layer Transition Measurement Techniques on a Laminar Flow Wing
2005
·
Andrea Vavra
, William Solomon
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
·
5
Distributed Exhaust Nozzles for Jet Noise Reduction
2001
·
K. K. Ahuja
, Richard Gaeta
, et al.
·
NASA Technical Reports Server (NASA)
·
5
Transonic Fan Tip-Flow Features Revealed by High Frequency Response Over-Tip Pressure Measurements
2008
·
Hyoun-Woo Shin
, William Solomon
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
·
4
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)
2024
·
Melissa Kozul
, Massimiliano Nardini
, et al.
·
Journal of Turbomachinery
·
3
PDF
CFD Design and Flight Test of a Swept Laminar Flow Control Wing
2018
·
Andrew Carpenter
, William Solomon
, et al.
·
AIAA Applied Aerodynamics Conference
·
2
Air Vehicles Technology Integration Program (AVTIP). Delivery Order 0020: Prediction of Manufacturing Tolerances for Laminar Flow
2005
·
Aaron Drake
, Anne M. Bender
, et al.
·
Defense Technical Information Center (DTIC)
·
2
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation
2024
·
Melissa Kozul
, Massimiliano Nardini
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
QCSEE — Design and Test Contributions to the Rise Open Fan Program
2024
·
Aspi Wadia
, Jan Schilling
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
Investigation of Spoiler Ailerons with and Without a Gap Behind the Spoiler on a 45 Degree Sweptback Wing-Fuselage Combination at Mach Numbers from 0.60 to 1.03
1953
·
William Solomon
, F E West
, et al.
·
NASA Technical Reports Server (NASA)
Effect of longitudinal wing position on the pressure characteristics at transonic speeds of a 45 degree sweptback wing-fuselage model
1953
·
William Solomon
, James W Schmeer
·
University of Michigan Library Repository
Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
1953
·
William Solomon
·
NASA STI Repository (National Aeronautics and Space Administration)
An Investigation of Propeller Vibrations Excited by Wing Wakes
1952
·
W.H. Gray
, William Solomon
·
NASA Technical Reports Server (NASA)
Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
1948
·
William Solomon
·
NASA STI Repository (National Aeronautics and Space Administration)
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Works count:
20
Citation count:
78
H-index:
6
I10-index:
2
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