风洞
校准
航天学
应变计
空气动力学
航空航天工程
海洋工程
航空学
机械工程
工程类
结构工程
物理
量子力学
出处
期刊:American Institute of Aeronautics and Astronautics, Inc. eBooks
[American Institute of Aeronautics and Astronautics, Inc.]
日期:2020-01-01
被引量:3
摘要
No AccessCalibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020)Published Online:21 Apr 2020https://doi.org/10.2514/4.106019.001SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail AboutAbstract: This document provides a recommended method for calibration and use of internal strain-gage balances in wind tunnel testing. The practices include terminology, axis system definition, balance calibration methods, matrix, and documentation. Use of this document will facilitate the exchange of information among users, suppliers, and other interested parties. FiguresReferencesRelatedDetailsCited byStatic Calibration and Dynamic Behaviour of a Six-Component Force Balance for Variable Pressure Water Tunnel Facilities9 January 2021 | Experimental Techniques, Vol. 45, No. 2 What's Popular Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020) CrossmarkInformationCopyright © 2020 by the American Institute of Aeronautics and AstronauticsCopyright © 2020 by the American Institute of Aeronautics and Astronautics TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAerospace EngineeringAerospace ManufacturersAerospace SciencesComputational Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsNumerical AnalysisSociety and Aerospace TechnologyWind Tunnels KeywordsTransonic Wind TunnelAerodynamic ForceRegression AnalysisCombined LoadingData Acquisition SystemTemperature EffectsComputing MethodsLangley Research CenterTemperature SensorsFatigue AnalysisPDF
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