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dc.contributor.authorKasimov, Aslan R.
dc.date.accessioned2016-02-04T13:14:45Z
dc.date.available2016-02-04T13:14:45Z
dc.date.issued2015-10-08
dc.date.submitted2013-10-11
dc.identifier.urihttp://hdl.handle.net/10754/595576
dc.description.abstractA detonation engine can detonate a mixture of fuel and oxidizer within a cylindrical detonation region to produce work. The detonation engine can have a first and a second inlet having ends fluidly connected from tanks to the detonation engine. The first and second inlets can be aligned along a common axis. The inlets can be connected to nozzles and a separator can be positioned between the nozzles and along the common axis.
dc.relation.urlhttp://appft.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PG01&p=1&u=%2Fnetahtml%2FPTO%2Fsrchnum.html&r=1&f=G&l=50&s1=%2220150285506%22.PGNR.&OS=DN/20150285506&RS=DN/20150285506
dc.relation.urlhttp://assignment.uspto.gov/#/search?adv=publNum:20150285506
dc.relation.urlhttp://www.google.com/patents/US20150285506
dc.relation.urlhttp://worldwide.espacenet.com/publicationDetails/biblio?CC=US&NR=2015285506A1&KC=A1&FT=D
dc.titleStanding detonation wave engine
dc.typePatent
dc.contributor.departmentComputer, Electrical and Mathematical Sciences and Engineering (CEMSE) Division
dc.contributor.departmentApplied Mathematics and Computational Science Program
dc.description.statusGranted Patent
dc.contributor.assigneeKing Abdullah University of Science and Technology
dc.description.countryUnited States
dc.identifier.patentnumberUS9841192B2
dc.identifier.applicationnumberUS 20150285506 A1
refterms.dateFOA2018-06-13T11:58:25Z


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