Zobrazeno 1 - 9
of 9
pro vyhledávání: '"William E. Lipford"'
Publikováno v:
Sensors, Vol 16, Iss 12, p 2062 (2016)
Detection of flow transition on aircraft surfaces and models can be vital to the development of future vehicles and computational methods for evaluating vehicle concepts. In testing at ambient conditions, IR thermography is ideal for this measurement
Externí odkaz:
https://doaj.org/article/904a4dc1b70342d89ca42f674cb69f6e
Autor:
Kyle Z. Goodman, Phillip A. Kreth, Brett F. Bathel, Neal Watkins, William E. Lipford, E. Lara Lash, Scott A. Berry, Stephen B. Jones, John D. Schmisseur, Christopher S. Combs
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::450de93628481a9fc39906cb5f42a824
https://doi.org/10.2514/6.2019-1939.c1
https://doi.org/10.2514/6.2019-1939.c1
Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
Autor:
John D. Schmisseur, Phillip A. Kreth, Stephen B. Jones, William E. Lipford, E. Lara Lash, A. Neal Watkins, Brett F. Bathel, Kyle Z. Goodman, Christopher S. Combs, Scott A. Berry
Publikováno v:
AIAA Scitech 2019 Forum.
This paper highlights results from a collaborative study performed by The University of Tennessee Space Institute (UTSI) and NASA Langley Research Center on the Shockwave/Boundary-Layer Interaction (SWBLI) generated by a cylindrical protuberance on a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::298c0adcb6fa9569181ad6f68820c31f
https://doi.org/10.2514/6.2019-1939
https://doi.org/10.2514/6.2019-1939
Autor:
Jim Crafton, William E. Lipford, James W. Gregory, Bradley D. Leighty, A. Neal Watkins, Kyle Z. Goodman
Publikováno v:
AIAA Journal. 54:206-215
This paper will present details of a pressure-sensitive paint system for measuring global surface pressures on rotor blades in simulated forward flight at the 14×22 ft subsonic tunnel at the NASA Langley Research Center. The system was designed to u
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::745821a617915ca1e2954dea0baeb098
https://doi.org/10.2514/1.j054191
https://doi.org/10.2514/1.j054191
Publikováno v:
Sensors (Basel, Switzerland)
Sensors, Vol 16, Iss 12, p 2062 (2016)
Sensors; Volume 16; Issue 12; Pages: 2062
Sensors, Vol 16, Iss 12, p 2062 (2016)
Sensors; Volume 16; Issue 12; Pages: 2062
Detection of flow transition on aircraft surfaces and models can be vital to the development of future vehicles and computational methods for evaluating vehicle concepts. In testing at ambient conditions, IR thermography is ideal for this measurement
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b5aee4df15173db59cd4003a7e3f607a
https://doi.org/10.3390/s16122062
https://doi.org/10.3390/s16122062
Autor:
Bradley D. Leighty, Jim Crafton, Alan Forlines, A. Neal Watkins, Thomas J. Juliano, Oliver D. Wong, James W. Gregory, Kyle Z. Goodman, William E. Lipford, Larry Goss
Publikováno v:
28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
This paper will present details of a Pressure Sensitive Paint (PSP) system for measuring global surface pressures on the tips of rotorcraft blades in simulated forward flight at the 14- x 22-Foot Subsonic Tunnel at the NASA Langley Research Center. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c184f9c7449f0433712a76e06454264b
https://doi.org/10.2514/6.2012-2756
https://doi.org/10.2514/6.2012-2756
Autor:
William E. Lipford, Edward A. Massey, W. K. Goad, Kyle Z. Goodman, Bradley D. Leighty, Donald M. Oglesby, Linda R. Goad, A. Neal Watkins
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
The Pressure Sensitive Paint (PSP) method was used to measure global surface pressures on a model at full-scale flight Reynolds numbers. In order to achieve these conditions, the test was carried out at the National Transonic Facility (NTF) operating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0352aae062cfca310d78e3512f59f68c
https://doi.org/10.2514/6.2009-421
https://doi.org/10.2514/6.2009-421
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Pressure Sensitive Paint (PSP) and Temperature Sensitive Paint (TSP) were used to visualize and quantify the surface interactions of reaction control system (RCS) jets on the aft body of capsule reentry vehicle shapes. The first model tested was an A
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47d7daed48dc42bc5fa716c98679b565
https://doi.org/10.2514/6.2008-1230
https://doi.org/10.2514/6.2008-1230
Autor:
Oliver D. Wong, D.M. Oglesby, J.L. Ingram, William E. Lipford, Bradley D. Leighty, Anthony Neal Watkins
Publikováno v:
2007 22nd International Congress on Instrumentation in Aerospace Simulation Facilities.
This paper describes the results from a proof of concept test to examine the feasibility of using pressure sensitive paint (PSP) to measure global surface pressures on rotorcraft blades in hover. The test was performed using the U.S. army 2-meter rot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::856e348ce76213c01b2820d17b655f7c
https://doi.org/10.1109/iciasf.2007.4380888
https://doi.org/10.1109/iciasf.2007.4380888