Zobrazeno 1 - 7
of 7
pro vyhledávání: '"William A. Lokos"'
Publikováno v:
AIAA Scitech 2019 Forum.
State-of-the-art instrumentation techniques have provided an opportunity to obtain greater insight into structural wing loads during flight. An investigation was undertaken to research new wing instrumentation and load sensing techniques for measurin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::767a71b053feba8fc6bbaafd332ac953
https://doi.org/10.2514/6.2019-0227
https://doi.org/10.2514/6.2019-0227
Autor:
Eric J. Miller, Andrew Holguin, Larry D. Hudson, William A. Lokos, David C. Neufeld, Ronnie Haraguchi
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
This paper describes the design and conduct of the strain-gage load calibration ground test of the SubsoniC Research Aircraft Testbed, Gulfstream III aircraft, and the subsequent data analysis and results. The goal of this effort was to create and va
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::753a56bf0e96f53440758e0e17ed2fd4
https://doi.org/10.2514/6.2015-2020
https://doi.org/10.2514/6.2015-2020
Autor:
Andrew M. Lizotte, William A. Lokos
Publikováno v:
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Traditional techniques in structural load measurement entail the correlation of a known load with strain-gage output from the individual components of a structure or machine. The use of strain gages has proved successful and is considered the standar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1cb639c6796910492d897a069980d3d3
https://doi.org/10.2514/6.2005-2016
https://doi.org/10.2514/6.2005-2016
Publikováno v:
SPIE Proceedings.
The initial concept and development of a low-cost, adaptable method for the measurement of static and dynamic aeroelastic deformation of aircraft during flight testing is presented. The method is adapted from a proven technique used in wind tunnel te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77b2848ab75def4e25fdaa3c1855333a
https://doi.org/10.1117/12.504157
https://doi.org/10.1117/12.504157
Publikováno v:
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The left wing of the Active Aeroelastic Wing (AAW) F/A-18 airplane has been ground-load-tested to quantify its torsional stiffness. The test has been performed at the NASA Dryden Flight Research Center in November 1996, and again in April 2001 after
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47470989aabcb8fc4ae7e2c0bd54c23b
https://doi.org/10.2514/6.2002-1333
https://doi.org/10.2514/6.2002-1333
Publikováno v:
6th AIAA Biennial Flight Test Conference.
The mission adaptive wing (MAW) consisted of leading- and trailing-edge variable-camber surfaces that could be deflected in flight to provide a near-ideal wing camber shape for any flight condition. These surfaces featured smooth, flexible upper surf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f64f0d52784d3c376ec4c37686946027
https://doi.org/10.2514/6.1992-4101
https://doi.org/10.2514/6.1992-4101
Conference
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