No AccessInfluence of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic ConeIan T. Neel, Andrew Leidy, Nathan R. Tichenor and Rodney D. BowersoxIan T. NeelTexas A&M UniversitySearch for more papers by this author, Andrew LeidyTexas A&M UniversitySearch for more papers by this author, Nathan R. TichenorTexas A&M UniversitySearch for more papers by this author and Rodney D. BowersoxTexas A&M UniversitySearch for more papers by this authorAIAA 2018-1821Session: Stability and Transition V: High-Speed ConesPublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-1821SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byLeading-Edge Curvature Influence on Hypersonic Boundary Layer TransitionJonathan L. Hill, Matthew P. Borg, Matthew W. Tufts, Elizabeth K. Benitez and Mark F. Reeder19 January 2023Tunnel Environment Effects on the single Fin-Cone at Mach 6John Wirth and Rodney D. Bowersox20 June 2022Tunnel Noise Effects on Hypersonic Cylinder-Induced Transitional Shock-Wave/Boundary-Layer InteractionsAndrew N. Leidy, Ian T. Neel, Nathan R. Tichenor, Rodney D. W. Bowersox and John D. Schmisseur23 April 2021 | AIAA Journal, Vol. 59, No. 7Preflight Ground Test Analyses of the Boundary Layer Transition (BOLT) Flight GeometryHeather E. Kostak and Rodney D. W. Bowersox1 October 2020 | Journal of Spacecraft and Rockets, Vol. 58, No. 1Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone14 December 2020 | Advances in Aerodynamics, Vol. 2, No. 1Engineering Model for Transition Prediction Based on a Hypersonic Quiet Wind TunnelMingtao Shi, Wenkai Zhu and Cunbiao Lee2 April 2020 | AIAA Journal, Vol. 58, No. 8Three-dimensionality in shock/boundary layer interactions: a numerical and experimental investigationAnubhav Dwivedi, Casey J. Broslawski, Graham V. Candler and Rodney D. Bowersox8 June 2020Some effects of tunnel noise on cylinder-induced Mach 6 transitional shock wave boundary layer interactionsAndrew Leidy, Ian T. Neel, Nathan R. Tichenor, Rodney D. Bowersox and John D. Schmisseur5 January 2020Using Discrete and Distributed Roughness to Generate Stationary Crossflow Waves in a Mach 6 Quiet TunnelJosh Edelman and Steven P. Schneider15 June 2019HIFiRE-5 Boundary-Layer Transition Measured in a Mach-6 Quiet Tunnel with Infrared ThermographyThomas J. Juliano, Laura A. Paquin and Matthew P. Borg11 January 2019 | AIAA Journal, Vol. 57, No. 5Effect of Wall Blowing on Hypersonic Boundary-Layer TransitionFernando Miró Miró, Pieter Dehairs, Fabio Pinna, Maria Gkolia, Davide Masutti, Tamas Regert and Olivier Chazot29 January 2019 | AIAA Journal, Vol. 57, No. 4Hypersonic Boundary Layer Cross Flow Transition - Characteristics and ControlThomas C. Corke and Rodney D. Bowersox7 January 2018 What's Popular 2018 AIAA Aerospace Sciences Meeting 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-1821 CrossmarkInformationCopyright © 2018 by Ian Neel, Andrew Leidy, Nathan Tichenor, Rodney Bowersox. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsAirspeedBoundary LayersComputational Fluid DynamicsFluid DynamicsSkin FrictionTurbulenceVortex DynamicsWind Tunnels KeywordsBoundary Layer TransitionVortex StructureFreestream ConditionsPressure TransducersHypersonic Wind TunnelsYawSurface RoughnessPolyether Ether KetoneFreestream TurbulenceTemperature Sensitive PaintPDF Topics Fluid Dynamics