Errors and Uncertainties in Derived Gust Velocities Extracted from Flight Data
2017; American Institute of Aeronautics and Astronautics; Volume: 54; Issue: 2 Linguagem: Inglês
10.2514/1.c033850
ISSN1533-3868
AutoresKamran Rokhsaz, Linda K. Kliment,
Tópico(s)Probabilistic and Robust Engineering Design
ResumoNo AccessEngineering NoteErrors and Uncertainties in Derived Gust Velocities Extracted from Flight DataKamran Rokhsaz and Linda K. KlimentKamran RokhsazWichita State University, Wichita, Kansas 67260*Professor, Department of Aerospace Engineering. Associate Fellow AIAA.Search for more papers by this author and Linda K. KlimentWichita State University, Wichita, Kansas 67260†Assistant Professor, Department of Aerospace Engineering. Member AIAA.Search for more papers by this authorPublished Online:11 Feb 2017https://doi.org/10.2514/1.C033850SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Wilson E. B., “Theory of an Aeroplane Encountering Gusts,” NACA Rept. 1, Part 2, 1915. Google Scholar[2] Anon., “Airworthiness Requirements for Aircraft,” Civil Aeronautics Board, Aeronautics Bulletin Amendment 7a, Oct. 1934. 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LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 54, Number 2March 2017Special Section on Cranked Arrow Wing Aerodynamics Project International II/F-16XL CrossmarkInformationCopyright © 2016 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0021-8669 (print) or 1533-3868 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAircraft Components and StructureAircraft Conceptual DesignAircraft DesignAircraft Operations and TechnologyAircraft Wing DesignAircraftsAirfoilCivil AircraftJet AircraftWing ConfigurationsWing Planforms KeywordsFlight DataLanding GearKüssner FunctionEquivalent AirspeedAtmospheric TurbulenceWing LoadingAspect RatioCessnaAngle of AttackCompressibilityPDF Received31 December 2015Accepted2 November 2016Published online11 February 2017
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