FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2014980001> ?p ?o ?g. }

• W2014980001 endingPage "1726" @default.
• W2014980001 startingPage "1721" @default.
• W2014980001 abstract "No AccessTechnical NoteInvestigation on Hypersonic Inlet Starting Process in Continuous Freejet Wind TunnelYi Wang, Zhenguo Wang, Jianhan Liang and Xiaoqiang FanYi WangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China*Science and Technology on Scramjet Laboratory.Search for more papers by this author, Zhenguo WangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China*Science and Technology on Scramjet Laboratory.Search for more papers by this author, Jianhan LiangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China*Science and Technology on Scramjet Laboratory.Search for more papers by this author and Xiaoqiang FanScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China*Science and Technology on Scramjet Laboratory.Search for more papers by this authorPublished Online:20 Oct 2014https://doi.org/10.2514/1.B35289SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Mahoney J., Inlets for Supersonic Missiles, AIAA Education Series, AIAA, New York, 1990, p. 1. Google Scholar[2] Curran E. and Murthy S., Scramjet Propulsion, Vol. 189, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000, p. 449. Google Scholar[3] Van Wie D., Kwok F. and Walsh R., “Starting Characteristics of Supersonic Inlets,” AIAA Paper 1996-2914, 1996. LinkGoogle Scholar[4] Hawkins W. and Marquart E., “Two-Dimensional Generic Inlet Unstart Detection at Mach 2.5–5.0,” AIAA Paper 1995-6019, 1995. LinkGoogle Scholar[5] Vinogradov V., Stepanov V. and Goldfeld M., “Experimental and Numerical Investigation of Two Concepts of the Hypersonic Inlet,” AIAA Paper 1995-2721, 1995. LinkGoogle Scholar[6] Smart M., Trexler C. and Goldman A., “A Combined Experimental/Computational Investigation of Rocket Based Combined Cycle Inlet,” AIAA Paper 2001-0671, 2011. Google Scholar[7] Wagner J., Valdivia A., Yuceil K., Clemens N. T. and Dolling D. S., “An Experimental Investigation of Supersonic Inlet Unstart,” AIAA Paper 2007-4352, 2007. LinkGoogle Scholar[8] Falempin F., Wendling E., Goldfeld M., Starov A. and Timofeev K., “Influence of Gas Injection and Combustion on Start and Characteristics of Inlet,” AIAA Paper 2008-2514, 2008. LinkGoogle Scholar[9] Lu F. and Marren D., Advanced Hypersonic Test Facilities, Vol. 198, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2002, p. 24. Google Scholar[10] McGregor R., Molder S. and Paisley T., “Hypersonic Inlet Flow Starting in the Gun Tunnel,” Investigation in the Fluid Dynamics of Scramjet Inlets, Ryerson Polytechnical Inst. and Univ. of Toronto, Canada, July 1992. Google Scholar[11] Fan X., “Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet,” Ph.D. Thesis, National Univ. of Defense Technology, Changsha, PRC, 2006, pp. 79–81 (in Chinese). Google Scholar[12] Voland R., Rock K., Huebner L., Witte D. W., Fischer K. E. and McClinton C. R., “Hyper-X Engine Design and Ground Test Program,” AIAA Paper 1998-1532, 1998. LinkGoogle Scholar[13] Wang Y., Liang J., Fan X., Liu W. and Wang Z., “Investigation on the Unstarted Flowfield of a Three-Dimensional Sidewall Compression Hypersonic Inlet,” AIAA Paper 2009-7404, 2009. Google Scholar Previous article Next article" @default.
• W2014980001 created "2016-06-24" @default.
• W2014980001 creator A5017356818 @default.
• W2014980001 creator A5061864670 @default.
• W2014980001 creator A5067365795 @default.
• W2014980001 creator A5086544638 @default.
• W2014980001 date "2014-11-01" @default.
• W2014980001 modified "2023-09-27" @default.
• W2014980001 title "Investigation on Hypersonic Inlet Starting Process in Continuous Freejet Wind Tunnel" @default.
• W2014980001 cites W1969155460 @default.
• W2014980001 cites W2071936016 @default.
• W2014980001 cites W2314898706 @default.
• W2014980001 cites W2316724643 @default.
• W2014980001 cites W2331432197 @default.
• W2014980001 cites W2333024369 @default.
• W2014980001 cites W2333639143 @default.
• W2014980001 cites W626275094 @default.
• W2014980001 doi "https://doi.org/10.2514/1.b35289" @default.
• W2014980001 hasPublicationYear "2014" @default.
• W2014980001 type Work @default.
• W2014980001 sameAs 2014980001 @default.
• W2014980001 citedByCount "12" @default.
• W2014980001 countsByYear W20149800012016 @default.
• W2014980001 countsByYear W20149800012017 @default.
• W2014980001 countsByYear W20149800012018 @default.
• W2014980001 countsByYear W20149800012019 @default.
• W2014980001 countsByYear W20149800012022 @default.
• W2014980001 countsByYear W20149800012023 @default.
• W2014980001 crossrefType "journal-article" @default.
• W2014980001 hasAuthorship W2014980001A5017356818 @default.
• W2014980001 hasAuthorship W2014980001A5061864670 @default.
• W2014980001 hasAuthorship W2014980001A5067365795 @default.
• W2014980001 hasAuthorship W2014980001A5086544638 @default.
• W2014980001 hasConcept C105923489 @default.
• W2014980001 hasConcept C122824865 @default.
• W2014980001 hasConcept C127413603 @default.
• W2014980001 hasConcept C146978453 @default.
• W2014980001 hasConcept C178790620 @default.
• W2014980001 hasConcept C178802073 @default.
• W2014980001 hasConcept C185592680 @default.
• W2014980001 hasConcept C205991772 @default.
• W2014980001 hasConcept C56278489 @default.
• W2014980001 hasConcept C60808876 @default.
• W2014980001 hasConcept C83104080 @default.
• W2014980001 hasConceptScore W2014980001C105923489 @default.
• W2014980001 hasConceptScore W2014980001C122824865 @default.
• W2014980001 hasConceptScore W2014980001C127413603 @default.
• W2014980001 hasConceptScore W2014980001C146978453 @default.
• W2014980001 hasConceptScore W2014980001C178790620 @default.
• W2014980001 hasConceptScore W2014980001C178802073 @default.
• W2014980001 hasConceptScore W2014980001C185592680 @default.
• W2014980001 hasConceptScore W2014980001C205991772 @default.
• W2014980001 hasConceptScore W2014980001C56278489 @default.
• W2014980001 hasConceptScore W2014980001C60808876 @default.
• W2014980001 hasConceptScore W2014980001C83104080 @default.
• W2014980001 hasIssue "6" @default.
• W2014980001 hasLocation W20149800011 @default.
• W2014980001 hasOpenAccess W2014980001 @default.
• W2014980001 hasPrimaryLocation W20149800011 @default.
• W2014980001 hasRelatedWork W1493550625 @default.
• W2014980001 hasRelatedWork W1541689723 @default.
• W2014980001 hasRelatedWork W1973529026 @default.
• W2014980001 hasRelatedWork W1993388401 @default.
• W2014980001 hasRelatedWork W2009254629 @default.
• W2014980001 hasRelatedWork W2162460384 @default.
• W2014980001 hasRelatedWork W265715879 @default.
• W2014980001 hasRelatedWork W3147677527 @default.
• W2014980001 hasRelatedWork W4214621893 @default.
• W2014980001 hasRelatedWork W2189253721 @default.
• W2014980001 hasVolume "30" @default.
• W2014980001 isParatext "false" @default.
• W2014980001 isRetracted "false" @default.
• W2014980001 magId "2014980001" @default.
• W2014980001 workType "article" @default.