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Anthony Watkins
Anthony Watkins
NASA Langley Research Center
Verified email at nasa.gov
Title
Cited by
Cited by
Year
Portable, low-cost, solid-state luminescence-based O2 sensor
AN Watkins, BR Wenner, JD Jordan, W Xu, JN Demas, FV Bright
Applied Spectroscopy 52 (5), 750-754, 1998
981998
Carbon nanotube-based sensor and method for detection of crack growth in a structure
JM Smits, MT Kite, TC Moore, RA Wincheski, JAL Ingram, AN Watkins, ...
US Patent 7,278,324, 2007
882007
Carbon nanotube-based sensor and method for continually sensing changes in a structure
JD Jordan, AN Watkins, DM Oglesby, JAL Ingram
US Patent 7,194,912, 2007
732007
Preliminary results from an experimental assessment of a natural laminar flow design method
MN Lynde, RL Campbell, MB Rivers, SA Viken, DT Chan, AN Watkins, ...
AIAA Scitech 2019 Forum, 2298, 2019
562019
Measuring surface pressures on rotor blades using pressure-sensitive paint
AN Watkins, BD Leighty, WE Lipford, KZ Goodman, J Crafton, JW Gregory
AIAA Journal 54 (1), 206-215, 2016
512016
Blade tip pressure measurements using pressure-sensitive paint
OD Wong, AN Watkins, KZ Goodman, J Crafton, A Forlines, L Goss, ...
Journal of the American Helicopter Society 63 (1), 1-11, 2018
482018
Effects of processing temperature on the oxygen quenching behavior of tris (4, 7′-diphenyl-1, 10′-phenanthroline) ruthenium (II) sequestered within sol-gel-derived xerogel films
GA Baker, BR Wenner, AN Watkins, FV Bright
Journal of sol-gel science and technology 17, 71-82, 2000
482000
Experimental investigation of the nasa common research model with a natural laminar flow wing in the nasa langley national transonic facility
MB Rivers, MN Lynde, RL Campbell, SA Viken, DT Chan, AN Watkins, ...
AIAA Scitech 2019 Forum, 2189, 2019
412019
Assessment of the national transonic facility for natural laminar flow testing
J Crouch, M Sutanto, D Witkowski, A Watkins, M Rivers, R Campbell
48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2010
412010
Pressure sensitive paint measurements on 15% scale rotor blades in hover
O Wong, A Watkins, JA Ingram
35th AIAA Fluid Dynamics Conference and Exhibit, 5008, 2005
352005
A parallel multiharmonic frequency-domain fluorometer for measuring excited-state decay kinetics following one-, two-, or three-photon excitation
AN Watkins, CM Ingersoll, GA Baker, FV Bright
Analytical chemistry 70 (16), 3384-3396, 1998
351998
Single wall carbon nanotube-based structural health sensing materials
AN Watkins, JL Ingram, JD Jordan, RA Wincheski, JM Smits, PA Williams
Proceedings of the NSTI Nanotechnology Conference and Trade Show (NSTI …, 2004
342004
Experimental measurement of RCS jet interaction effects on a capsule entry vehicle
G Buck, A Watkins, P Danehy, J Inman, D Alderfer, A Dyakonov
46th AIAA Aerospace Sciences Meeting and Exhibit, 1229, 2008
312008
Static and time-resolved fluorescence of fluorescein-labeled dextran dissolved in aqueous solution or sequestered within a sol–gel-derived hydrogel
GA Baker, A áNeal Watkins, FV Bright
Analyst 124 (3), 373-379, 1999
311999
Hypersonic laminar boundary layer velocimetry with discrete roughness on a flat plate
B Bathel, P Danehy, J Inman, A Watkins, S Jones, W Lipford, K Goodman, ...
40th Fluid Dynamics Conference and Exhibit, 4998, 2010
302010
Non-intrusive measurements of a four-bladed rotor in hover—a first look
OD Wong, KW Noonan, AN Watkins, LN Jenkins, C Yao
American helicopter society aeromechanics specialists’ conference, 20-22, 2010
292010
Using pressure-and temperature-sensitive paint on the aftbody of a capsule entry vehicle
AN Watkins, GM Buck, BD Leighty, WE Lipford, DM Oglesby
AIAA journal 47 (4), 821-829, 2009
282009
Development of next generation lifetime PSP imaging systems
AN Watkins, JD Jordan, BD Leighty, JL Ingram, DM Oglesby
20th International Congress on Instrumentation in Aerospace Simulation …, 2003
282003
An optical technique for detecting fatigue cracks in aerospace structures
D Banaszak, GA Dale, AN Watkins, JD Jordan
ICIASF 99. 18th International Congress on Instrumentation in Aerospace …, 1999
251999
Boundary-layer detection at cryogenic conditions using temperature sensitive paint coupled with a carbon nanotube heating layer
KZ Goodman, WE Lipford, AN Watkins
Sensors 16 (12), 2062, 2016
232016
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