Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Keith C. Lynn"'
Publikováno v:
Journal of Aircraft. 52:1736-1755
Recent wind-tunnel tests at the NASA Langley Research Center National Transonic Facility used high-pressure bellows to route air to the semispan model for evaluating aircraft circulation control testing techniques. The introduction of these bellows w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e9c7878e263134586589025f7e36d5d
https://doi.org/10.2514/1.c032942
https://doi.org/10.2514/1.c032942
Publikováno v:
Journal of Aircraft. 52:884-889
The current approach used to apply uncertainty intervals to balance estimated loads is based on the root mean square error from calibration. Using the root mean square error, a constant interval is applied around the estimated load and it is expected
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::587db8cae30bbe68f0160d4748cb37d0
https://doi.org/10.2514/1.c032930
https://doi.org/10.2514/1.c032930
Publikováno v:
Journal of Aircraft. 52:638-649
Experimental design considerations for the development of calibration load schedules are discussed for the characterization of traditional five-component semispan balances used in aerodynamic ground testing applications. Detail is given on traditiona
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98d0452cce0154228087cccd29fd8148
https://doi.org/10.2514/1.c032811
https://doi.org/10.2514/1.c032811
Publikováno v:
Journal of Aircraft. 49:556-565
Wind-tunnel research was recently conducted at the NASA Langley Research Center s 31-Inch Mach 10 Hypersonic Facility in support of the Mars Science Laboratory s aerodynamic program. Researchers were interested in understanding the interaction betwee
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eb56c7cdee32096181e07c8f3e2067b8
https://doi.org/10.2514/1.c031567
https://doi.org/10.2514/1.c031567
Publikováno v:
31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::976ab7230aaf8c37bc1fcfb71de850b0
https://doi.org/10.2514/6.2015-3380
https://doi.org/10.2514/6.2015-3380
Autor:
Genevieve Dixon, Keith C. Lynn
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Force transducer designs used in the ground testing aeronautics community have seen minimal change over the last few decades. With increased focus on data quality and long-term performance capabilities over the life of these instruments, it is critic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79b3589b08e83a159f48b065a307a22f
https://doi.org/10.2514/6.2015-1789
https://doi.org/10.2514/6.2015-1789
Publikováno v:
52nd Aerospace Sciences Meeting.
Recent wind-tunnel tests at the NASA Langley Research Center National Transonic Facility utilized high-pressure bellows to route air to the semi-span model for evaluating aircraft circulation control testing techniques. The introduction of these bell
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0929e9489e9c02f5850fa31386822fd2
https://doi.org/10.2514/6.2014-0275
https://doi.org/10.2514/6.2014-0275
Publikováno v:
52nd Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed276279766c9edba620bcc9f610e238
https://doi.org/10.2514/6.2014-0276
https://doi.org/10.2514/6.2014-0276
Autor:
Keith C. Lynn, Michael J. Acheson, Scott L. Goodliff, William E. Milholen, Ray D. Rhew, Gregory S. Jones
Publikováno v:
28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
Recent wind-tunnel tests at the NASA Langley Research Center National Transonic Facility utilized high-pressure bellows to route air to the model for evaluating aircraft circulation control. The introduction of these bellows within the Sidewall Model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44aa309007ba810c6d1c4e9dde1e8bb9
https://doi.org/10.2514/6.2012-3318
https://doi.org/10.2514/6.2012-3318
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Wind tunnel research at NASA Langley Research Center s 31-inch Mach 10 hypersonic facility utilized a 5-component force balance, which provided a pressurized flow-thru capability to the test article. The goal of the research was to determine the inte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c89d061051b1503acb6b8a15b7ffe352
https://doi.org/10.2514/6.2011-950
https://doi.org/10.2514/6.2011-950