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• W4362472169 abstract "No AccessTechnical NotesDebris Blocker and Flow Terminator for a Shock TunnelBen A. Segall, David Shekhtman, Ahsan Hameed, James H. Chen, Alex R. Dworzanczyk and Nicholaus J. ParzialeBen A. Segall https://orcid.org/0000-0002-2259-0625Stevens Institute of Technology, Hoboken, New Jersey 07030*Graduate Student, Mechanical Engineering, Castle Point on Hudson.Search for more papers by this author, David ShekhtmanStevens Institute of Technology, Hoboken, New Jersey 07030†Postdoctoral Researcher, Mechanical Engineering, Castle Point on Hudson.Search for more papers by this author, Ahsan Hameed https://orcid.org/0000-0001-9563-3959Stevens Institute of Technology, Hoboken, New Jersey 07030*Graduate Student, Mechanical Engineering, Castle Point on Hudson.Search for more papers by this author, James H. ChenStevens Institute of Technology, Hoboken, New Jersey 07030*Graduate Student, Mechanical Engineering, Castle Point on Hudson.Search for more papers by this author, Alex R. DworzanczykStevens Institute of Technology, Hoboken, New Jersey 07030*Graduate Student, Mechanical Engineering, Castle Point on Hudson.Search for more papers by this author and Nicholaus J. ParzialeStevens Institute of Technology, Hoboken, New Jersey 07030‡Associate Professor, Mechanical Engineering, Castle Point on Hudson; . Senior Member AIAA (Corresponding Author).Search for more papers by this authorPublished Online:31 Mar 2023https://doi.org/10.2514/1.J062348SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Leyva I. 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G., “Gasdynamical Detectors of Driver Gas Contamination in a High-Enthalpy Shock Tunnel,” AIAA Journal, Vol. 36, No. 3, 1998, pp. 313–319. https://doi.org/10.2514/2.383 LinkGoogle Scholar[24] Sudani N., Valiferdowsi B. and Hornung H. G., “Test Time Increase by Delaying Driver Gas Contamination for Reflected Shock Tunnels,” AIAA Journal, Vol. 38, No. 9, 2000, pp. 1497–1503. https://doi.org/10.2514/2.1138 LinkGoogle Scholar[25] Hannemann K., Schneider M., Reimann B. and Schramm J. M., “The Influence and Delay of Driver Gas Contamination in HEG,” 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, AIAA Paper 2000-2593, 2000, pp. 1–14. https://doi.org/10.2514/6.2000-2593 Google Scholar[26] Olivier H., “The Aachen Shock Tunnel TH2 with Dual Driver Mode Operation,” Experimental Methods of Shock Wave Research, Springer, New York, 2016, pp. 111–129. https://doi.org/10.1007/978-3-319-23745-9_5 Google Scholar[27] Goozée R. J., Seal P. A. and Saxena D. R., “Simulation of a Complete Reflected Shock Tunnel Showing a Vortex Mechanism for Flow Contamination,” Shock Waves, Vol. 15, Nos. 3–4, 2006, pp. 165–176. https://doi.org/10.1007/s00193-006-0015-4 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Articles in Advance CrossmarkInformationCopyright © 2023 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 eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronauticsAerospace SciencesFlow Control ValvesFlow Diagnostics and ControlFlow RegimesFluid DynamicsFluid Mechanics KeywordsFreestream Mach NumberFluid MechanicsFlow ConditionsPressure Relief ValveCenterbodyNozzle Flow TerminatorHypersonic Ground TestingShock TunnelsMach 6Flow QualityAcknowledgmentsBen A. Segall, David Shekhtman, Ahsan Hameed, James H. Chen, Alex R. Dworzanczyk, and Nicholaus J. Parziale were supported by U.S. Office of Naval Research and U.S. Air Force Office of Scientific Research (AFOSR) grants, including N00014-19-1-2523, N00014-20-1-2637, N00014-20-1-2682, N00014-20-1-2549, FA9550-18-1-0403, and FA9550-19-1-0182. We thank Eric Marineau and the U.S. Office of Naval Research for sponsoring the construction and development of the Stevens Shock Tunnel. We also thank AFOSR Program Manager Sarah Popkin for her support.PDF Received17 August 2022Accepted1 March 2023Published online31 March 2023" @default.
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