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Neal Watkins
Observed name:
Watkins, Neal
Institution:
Langley Research Center
Observed institutions:
Lockheed Martin (United States),
Langley Research Center
OpenAlex ID:
A5028613319
Transition Detection at Cryogenic Temperatures Using a Carbon-Based Resistive Heating Layer Coupled with Temperature Sensitive Paint
2019
·
Neal Watkins
, Kyle Z. Goodman
, et al.
·
AIAA SciTech Forum
·
16
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
Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness
2021
·
James C. Ross
, Marie Denison
, et al.
·
AIAA AVIATION Forum
·
6
Flight Test of a Resistive Heating Coating for Visualizing Flow Transition
2020
·
Neal Watkins
, Sarah Peak
, et al.
·
AIAA AVIATION Forum
·
5
Controlled Deposition and Applied Field Alignment of Single Walled Carbon Nanotubes for CNT Device Fabrication.
2002
·
Jan Smits
, Buzz Wincheski
, et al.
·
MRS Proceedings
·
4
Implementation of an Unsteady PSP System in the NASA Transonic Dynamics Tunnel
2022
·
Daniel Reese
, Sarah Peak
, et al.
·
AIAA AVIATION Forum
·
3
Application of PSP on the SWiFT Model in the National Transonic Facility
2025
·
Neal Watkins
, Daniel Reese
, et al.
·
AIAA SciTech Forum
·
2
Testing of the Trim Tab Parametric Model in NASA Langley’s Unitary Plan Wind Tunnel
2013
·
Kelly J. Murphy
, Ashley M. Korzun
, et al.
·
AIAA Applied Aerodynamics Conference
·
2
PDF
Nanomanipulation and Lithography for Carbon Nanotube Based Nondestructive Evaluation Sensor Development
2002
·
Buzz Wincheski
, J.M.M. Smits
, et al.
·
NASA STI Repository (National Aeronautics and Space Administration)
·
2
PDF
Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
2019
·
Brett F. Bathel
, Stephen B. Jones
, et al.
·
AIAA SciTech Forum
·
1
Withdrawal: Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
2019
·
Brett F. Bathel
, Stephen B. Jones
, et al.
·
AIAA SciTech Forum
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Works count:
12
Citation count:
54
H-index:
4
I10-index:
2
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