Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft

Min Chang; Weixiang Zhou; Bo Peng; Junqiang Bai

doi:10.1007/978-981-13-3305-7_96

Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft

Min Chang, Weixiang Zhou, Bo Peng, Junqiang Bai

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

This paper carries out a modeling method of ducted propulsion system of vertical take-off and landing aircraft. On axial flow condition, the model of ducted propulsion system, based momentum theory, is established and verified. Based on the non-dimensional definition of open propeller, the non-dimensional method, applied to the ducted blades, is proposed. The research shows that the ducted propulsion system model and the ducted blade non-dimensional method are reasonable and effective, for high performance aircraft configuration design with tilting duct-fan propulsion system.

Original language	English
Title of host publication	The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
Editors	Xinguo Zhang
Publisher	Springer Verlag
Pages	1222-1230
Number of pages	9
ISBN (Print)	9789811333040
DOIs	https://doi.org/10.1007/978-981-13-3305-7_96
State	Published - 2019
Event	Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 - Chengdu, China Duration: 16 Oct 2018 → 18 Oct 2018

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	459
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
Country/Territory	China
City	Chengdu
Period	16/10/18 → 18/10/18

Keywords

Ducted propulsion system
Modeling method
Momentum theory
Non-dimensional method
Vertical take-off and landing aircraft

Access to Document

10.1007/978-981-13-3305-7_96

Cite this

Chang, M., Zhou, W., Peng, B., & Bai, J. (2019). Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft. In X. Zhang (Ed.), The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 (pp. 1222-1230). (Lecture Notes in Electrical Engineering; Vol. 459). Springer Verlag. https://doi.org/10.1007/978-981-13-3305-7_96

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title = "Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft",

abstract = "This paper carries out a modeling method of ducted propulsion system of vertical take-off and landing aircraft. On axial flow condition, the model of ducted propulsion system, based momentum theory, is established and verified. Based on the non-dimensional definition of open propeller, the non-dimensional method, applied to the ducted blades, is proposed. The research shows that the ducted propulsion system model and the ducted blade non-dimensional method are reasonable and effective, for high performance aircraft configuration design with tilting duct-fan propulsion system.",

keywords = "Ducted propulsion system, Modeling method, Momentum theory, Non-dimensional method, Vertical take-off and landing aircraft",

author = "Min Chang and Weixiang Zhou and Bo Peng and Junqiang Bai",

note = "Publisher Copyright: {\textcopyright} 2019, Springer Nature Singapore Pte Ltd.; Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 ; Conference date: 16-10-2018 Through 18-10-2018",

year = "2019",

doi = "10.1007/978-981-13-3305-7_96",

language = "英语",

isbn = "9789811333040",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Verlag",

pages = "1222--1230",

editor = "Xinguo Zhang",

booktitle = "The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018",

}

Chang, M, Zhou, W, Peng, B & Bai, J 2019, Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft. in X Zhang (ed.), The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. Lecture Notes in Electrical Engineering, vol. 459, Springer Verlag, pp. 1222-1230, Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018, Chengdu, China, 16/10/18. https://doi.org/10.1007/978-981-13-3305-7_96

Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft. / Chang, Min; Zhou, Weixiang; Peng, Bo et al.
The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. ed. / Xinguo Zhang. Springer Verlag, 2019. p. 1222-1230 (Lecture Notes in Electrical Engineering; Vol. 459).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Peng, Bo

AU - Bai, Junqiang

PY - 2019

Y1 - 2019

N2 - This paper carries out a modeling method of ducted propulsion system of vertical take-off and landing aircraft. On axial flow condition, the model of ducted propulsion system, based momentum theory, is established and verified. Based on the non-dimensional definition of open propeller, the non-dimensional method, applied to the ducted blades, is proposed. The research shows that the ducted propulsion system model and the ducted blade non-dimensional method are reasonable and effective, for high performance aircraft configuration design with tilting duct-fan propulsion system.

AB - This paper carries out a modeling method of ducted propulsion system of vertical take-off and landing aircraft. On axial flow condition, the model of ducted propulsion system, based momentum theory, is established and verified. Based on the non-dimensional definition of open propeller, the non-dimensional method, applied to the ducted blades, is proposed. The research shows that the ducted propulsion system model and the ducted blade non-dimensional method are reasonable and effective, for high performance aircraft configuration design with tilting duct-fan propulsion system.

KW - Ducted propulsion system

KW - Modeling method

KW - Momentum theory

KW - Non-dimensional method

KW - Vertical take-off and landing aircraft

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Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft

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