{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,2,21]],"date-time":"2025-02-21T20:19:00Z","timestamp":1740169140213,"version":"3.37.3"},"reference-count":31,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2019,1,1]],"date-time":"2019-01-01T00:00:00Z","timestamp":1546300800000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/legalcode"}],"funder":[{"DOI":"10.13039\/501100002663","name":"Northwestern Polytechnical University","doi-asserted-by":"publisher","award":["3102019JC009"],"award-info":[{"award-number":["3102019JC009"]}],"id":[{"id":"10.13039\/501100002663","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Access"],"published-print":{"date-parts":[[2019]]},"DOI":"10.1109\/access.2019.2949062","type":"journal-article","created":{"date-parts":[[2019,10,23]],"date-time":"2019-10-23T20:26:23Z","timestamp":1571862383000},"page":"155184-155193","source":"Crossref","is-referenced-by-count":5,"title":["Blended Wing Body Thrust Reverser Cascade Feasibility Evaluation Through CFD"],"prefix":"10.1109","volume":"7","author":[{"ORCID":"https:\/\/orcid.org\/0000-0001-8095-9569","authenticated-orcid":false,"given":"Yu","family":"Gang","sequence":"first","affiliation":[]},{"given":"Li","family":"Dong","sequence":"additional","affiliation":[]},{"given":"Chen","family":"Zhenli","sequence":"additional","affiliation":[]},{"given":"Zhang","family":"Zeyu","sequence":"additional","affiliation":[]}],"member":"263","reference":[{"article-title":"Impact of ultra-high bypass\/hybrid wing body integration on propulsion system performance and operability (invited)","year":"0","author":"lord","key":"ref31"},{"article-title":"Transonic 3-D euler analysis of flows around fanjet engine and TPS. Comparison with wind tunnel experiment, evaluation of TPS testing method and 3-D flow","year":"1989","author":"hirose","key":"ref30"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.2514\/6.2001-3747"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2015.02.015"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.2514\/6.1998-438"},{"key":"ref13","doi-asserted-by":"crossref","first-page":"1599","DOI":"10.2514\/1.C000214","article-title":"Potential effects of blended wing bodies on the air transportation system","volume":"47","author":"mart\u00ednezval","year":"2015","journal-title":"J Aircr"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.2514\/6.2016-0011"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.2514\/6.2012-5649"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1016\/S1270-9638(01)01139-7"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.2514\/6.2003-934"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2017.09.037"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1016\/j.paerosci.2015.12.002"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.2514\/3.12149"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.2514\/6.2012-3919"},{"key":"ref27","first-page":"1239","article-title":"Engine and installation configurations for a silent aircraft","volume":"58","author":"hall","year":"2005","journal-title":"Amer J Hum Genet"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.1109\/ICMA.2011.5986275"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1016\/j.proeng.2011.10.075"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.2514\/6.1989-1835"},{"journal-title":"The Jet Engine","first-page":"159","year":"1996","key":"ref5"},{"key":"ref8","first-page":"974","article-title":"Review of thrust reverser mechanism used in turbofan jet engine aircraft","volume":"6","author":"siddiqui","year":"2013","journal-title":"Int J Eng Res Technol"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.3182\/20120620-3-DK-2025.00077"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.1108\/EC-05-2016-0163"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.2514\/6.2003-6748"},{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.1109\/TTE.2015.2426499"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.2514\/6.2017-0098"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.2514\/6.2012-838"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.2514\/6.2006-1323"},{"article-title":"Blended wing body (BWB) boundary layer ingestion (BLI) inlet configuration and system studies","year":"2006","author":"kawai","key":"ref24"},{"article-title":"Engine design implications for a blended wing-body airplane with boundary later ingestion","year":"2003","author":"hanlon","key":"ref23"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.2514\/1.9084"},{"article-title":"Experimental investigation of boundary layer ingestion into diffusing inlets","year":"1999","author":"anabtawi","key":"ref25"}],"container-title":["IEEE Access"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/6287639\/8600701\/08880660.pdf?arnumber=8880660","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2021,8,10]],"date-time":"2021-08-10T19:40:59Z","timestamp":1628624459000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/8880660\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2019]]},"references-count":31,"URL":"https:\/\/doi.org\/10.1109\/access.2019.2949062","relation":{},"ISSN":["2169-3536"],"issn-type":[{"type":"electronic","value":"2169-3536"}],"subject":[],"published":{"date-parts":[[2019]]}}}