{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,6,25]],"date-time":"2026-06-25T20:46:19Z","timestamp":1782420379175,"version":"3.54.5"},"reference-count":55,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2026,1,1]],"date-time":"2026-01-01T00:00:00Z","timestamp":1767225600000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2026,1,1]],"date-time":"2026-01-01T00:00:00Z","timestamp":1767225600000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2026,1,1]],"date-time":"2026-01-01T00:00:00Z","timestamp":1767225600000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-037"}],"funder":[{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"publisher","award":["52572420"],"award-info":[{"award-number":["52572420"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]},{"name":"National Key Laboratory of Aircraft Configuration Design","award":["JBGS-202502"],"award-info":[{"award-number":["JBGS-202502"]}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Trans. Aerosp. Electron. Syst."],"published-print":{"date-parts":[[2026]]},"DOI":"10.1109\/taes.2026.3689077","type":"journal-article","created":{"date-parts":[[2026,4,29]],"date-time":"2026-04-29T19:54:12Z","timestamp":1777492452000},"page":"10427-10445","source":"Crossref","is-referenced-by-count":0,"title":["Multipoint Inverse Design Method for an Integrated Tail-Propulsive Propeller in Canard Rotor-Wing UAV"],"prefix":"10.1109","volume":"62","author":[{"ORCID":"https:\/\/orcid.org\/0009-0009-1639-9902","authenticated-orcid":false,"given":"Zhengang","family":"Zhang","sequence":"first","affiliation":[{"name":"Northwestern Polytechnical University, Xi’an, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-2049-7793","authenticated-orcid":false,"given":"Huan","family":"Zhao","sequence":"additional","affiliation":[{"name":"Northwestern Polytechnical University, Xi’an, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Shekun","family":"Wang","sequence":"additional","affiliation":[{"name":"Northwestern Polytechnical University, Xi’an, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Kaiyuan","family":"Fan","sequence":"additional","affiliation":[{"name":"Northwestern Polytechnical University, Xi’an, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Zhenghong","family":"Gao","sequence":"additional","affiliation":[{"name":"Northwestern Polytechnical University, Xi’an, China"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"263","reference":[{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.1109\/aero47225.2020.9172554"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.1109\/codit49905.2020.9263896"},{"issue":"01","key":"ref3","first-page":"179","article-title":"Conceptual design study of compound VTOL aircraft with rotor\/fixed-wing integration","volume":"37","author":"Zhang","year":"2016","journal-title":"Acta Aeronautica ET Astronautica Sinica"},{"issue":"02","key":"ref4","first-page":"127","article-title":"Development trends and evolutionary analysis of vertical takeoff and landing aircraft","volume-title":"Adv. Aeronautical Sci. Eng.","volume":"6","author":"Liu","year":"2015"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1109\/access.2022.3207282"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1016\/j.proeng.2017.07.187"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.1109\/icepe.2014.6970074"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.1016\/j.petrol.2021.109633"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.4050\/jahs.67.032005"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.3390\/app11083385"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1108\/ijius-01-2019-0001"},{"key":"ref12","first-page":"3","article-title":"A review of configuration design for distributed propulsion transitioning VTOL aircraft","volume-title":"Proc. Asia-Pacific Int. Symp. Aerosp. Technol.","author":"Finger","year":"2017"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.3390\/aerospace6030026"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.2514\/6.2011-6940"},{"key":"ref15","article-title":"Research on rotor technology for novel rotary-wing aircraft","author":"Deng","year":"2006"},{"issue":"08","key":"ref16","first-page":"2498","article-title":"Interference aerodynamic characteristics of rotary-wing aircraft in rotor-mode forward flight","volume":"37","author":"Sun","year":"2016","journal-title":"Acta Aeronautica ET Astronautica Sinica"},{"issue":"02","key":"ref17","first-page":"232","article-title":"Aerodynamic characteristics of rotary-wing aircraft in hover","volume":"33","author":"Sun","year":"2015","journal-title":"Acta Aerodynamica Sinica"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1016\/j.cja.2019.04.002"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1109\/access.2019.2917316"},{"issue":"04","key":"ref20","first-page":"74","article-title":"Design, manufacture and airworthiness test of a certain type of electric aircraft propeller","volume":"1","author":"Ma","year":"2023","journal-title":"Green Energy Aviation"},{"issue":"01","key":"ref21","first-page":"136","article-title":"A design method for high efficiency propeller","volume":"30","author":"Xiang","year":"2015","journal-title":"J. Aerosp. Power"},{"key":"ref22","article-title":"Research on the design, optimization and verification technology of high-efficiency propellers for power gliders","author":"Zhang","year":"2022"},{"issue":"04","key":"ref23","first-page":"8390+123","article-title":"Method of high-efficiency propeller for solar-powered UAV in low altitude","volume":"13","author":"Qiu","year":"2022","journal-title":"Adv. Aeronautical Sci. Eng."},{"issue":"05","key":"ref24","first-page":"513","article-title":"Aerodynamic design research of tilt-propeller aircraft blades","author":"Luo","year":"2002","journal-title":"J. Aerosp. Power"},{"issue":"03","key":"ref25","first-page":"2731+46","article-title":"Design and performance analysis of propeller for tilt rotor UAV","volume":"35","author":"Wu","year":"2018","journal-title":"J. Shenyang Aerosp. Univ."},{"issue":"03","key":"ref26","first-page":"322","article-title":"Aerodynamic optimization design of micro air vehicle propellers","author":"Luo","year":"2003","journal-title":"J. Nanjing Univ. Aeronaut. Astronaut."},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.2514\/6.2023-2612"},{"issue":"12","key":"ref28","first-page":"101","article-title":"Integrated design methodology for tilt-ducted propellers","volume":"39","author":"Chen","year":"2024","journal-title":"J. Aerosp. Power"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2024.108963"},{"issue":"09","key":"ref30","first-page":"100","article-title":"Aerodynamic optimization method of propeller multi-design points and variable pitch angle strategy","volume":"45","author":"Wang","year":"2024","journal-title":"Acta Aeronautica ET Astronautica Sinica"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2025.109967"},{"key":"ref32","doi-asserted-by":"publisher","DOI":"10.3390\/aerospace9030153"},{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.5614\/j.eng.technol.sci.2024.56.3.8"},{"key":"ref34","article-title":"Estimation of aerodynamic loads of a propeller through improved blade element and momentum theory and propeller design optimization","author":"Kaya","year":"2021"},{"key":"ref35","doi-asserted-by":"publisher","DOI":"10.2514\/6.2023-3590"},{"key":"ref36","doi-asserted-by":"publisher","DOI":"10.3390\/machines13060490"},{"key":"ref37","doi-asserted-by":"publisher","DOI":"10.1016\/j.cja.2025.103481"},{"key":"ref38","doi-asserted-by":"publisher","DOI":"10.1016\/j.rineng.2025.104573"},{"key":"ref39","doi-asserted-by":"publisher","DOI":"10.2514\/6.2023-0026"},{"key":"ref40","doi-asserted-by":"publisher","DOI":"10.4271\/790585"},{"key":"ref41","first-page":"445","article-title":"A procedure for propeller design by inverse methods","volume-title":"Proc. Int. Conf. Inverse Des. Concepts Eng. Sci.","author":"Eppler","year":"1984"},{"key":"ref42","doi-asserted-by":"publisher","DOI":"10.1017\/s0001924000096068"},{"key":"ref43","doi-asserted-by":"publisher","DOI":"10.2514\/6.2007-7754"},{"key":"ref44","doi-asserted-by":"publisher","DOI":"10.1061\/(asce)as.1943-5525.0000055"},{"key":"ref45","doi-asserted-by":"publisher","DOI":"10.1177\/0954410011415476"},{"key":"ref46","doi-asserted-by":"publisher","DOI":"10.2514\/1.c034023"},{"issue":"01","key":"ref47","first-page":"136","article-title":"A high-efficiency propeller design method","volume":"30","author":"Xiang","year":"2015","journal-title":"J. Aerosp. Power"},{"issue":"05","key":"ref48","first-page":"1033","article-title":"Design and aerodynamic performance analysis of a type of UAV propeller","volume":"36","author":"He","year":"2021","journal-title":"J. Aerosp. Power"},{"key":"ref49","article-title":"Research on the design and verification method of propeller for hydrogen energy general-purpose aircraft","author":"Wu","year":"2023"},{"key":"ref50","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2018.05.008"},{"issue":"02","key":"ref51","first-page":"434","article-title":"A propeller design method for arbitrarily prescribed circulation distribution","volume":"34","author":"Fan","year":"2019","journal-title":"J. Aerosp. Power"},{"issue":"06","key":"ref52","first-page":"1238","article-title":"A method of propeller design with given thrust distribution and its application","volume":"35","author":"Guo","year":"2020","journal-title":"J. Aerosp. Power"},{"issue":"08","key":"ref53","first-page":"1901","article-title":"Propeller design rule extraction based on rough set theory","volume":"38","author":"Hu","year":"2023","journal-title":"J. Aerosp. Power"},{"issue":"02","key":"ref54","first-page":"209","article-title":"Engineering methods for improving efficiency of small UAV propellers","volume":"22","author":"Ma","year":"2004","journal-title":"J. Northwestern Polytechnical Univ."},{"issue":"03","key":"ref55","first-page":"460","article-title":"Design and test of a propeller for an electric aircraft","volume":"34","author":"Xiang","year":"2016","journal-title":"J. Northwestern Polytechnical Univ."}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx8\/7\/11316225\/11501215.pdf?arnumber=11501215","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2026,6,25]],"date-time":"2026-06-25T19:46:39Z","timestamp":1782416799000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/11501215\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2026]]},"references-count":55,"URL":"https:\/\/doi.org\/10.1109\/taes.2026.3689077","relation":{},"ISSN":["0018-9251","1557-9603","2371-9877"],"issn-type":[{"value":"0018-9251","type":"print"},{"value":"1557-9603","type":"electronic"},{"value":"2371-9877","type":"electronic"}],"subject":[],"published":{"date-parts":[[2026]]}}}