No AccessUpgrades to the Texas A&M Oran W. Nicks Low-Speed Wind Tunnel for M=0.4 OperationAlexander P. Herring, Douglas Kutz, Lisa Brown and Edward B. WhiteAlexander P. HerringTexas A&M UniversitySearch for more papers by this author, Douglas KutzTexas A&M UniversitySearch for more papers by this author, Lisa BrownTexas A&M UniversitySearch for more papers by this author and Edward B. WhiteTexas A&M UniversitySearch for more papers by this authorAIAA 2015-2864Session: Ground Test Facility Improvements IPublished Online:19 Jun 2015https://doi.org/10.2514/6.2015-2864SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byWind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with FlapC. P. van Dam, Sai Bharath Mothukuri, Seyedeh Sheida Hosseini, Edward B. White , Lisa M. Brown, Douglas M. Kutz and Ezequiel Justiniano1 November 2022 | Journal of Aircraft, Vol. 60, No. 2Wind Tunnel Experiment of Microjet-based Flow Control on a Multi-Element High-Lift AirfoilCase P. Van Dam, Sai B. Mothukuri, Seyedeh Sheida Hosseini, Edward White, Lisa Brown, Doug Kutz and Ezequiel Justiniano29 December 2021 What's Popular 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference 22-26 June 2015Dallas, TXhttps://doi.org/10.2514/6.2015-2864 CrossmarkInformationCopyright © 2015 by Alexander Herring, Douglas Kutz, Lisa Brown and Edward White. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsFlow Diagnostics and ControlFlow RegimesFluid DynamicsFluid MechanicsSkin FrictionVortex DynamicsWind Tunnels KeywordsLow Speed Wind TunnelAerodynamic ForceDynamic PressureStatic PressureYawData Acquisition SystemSkin FrictionAngle of AttackPressure ProbesNASA LangleyPDF Topics Ground Testing