Research on aerodynamic characteristics of morphing aircraft with a telescopic wing

Xi You Zhao; Jun Hu

doi:10.4028/www.scientific.net/AMR.709.257

Research on aerodynamic characteristics of morphing aircraft with a telescopic wing

Xi You Zhao
, Jun Hu

School of Aerospace Engineering

Beijing Institute of Technology

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

Abstract

A kind of morphing aircraft based on the concept of telescopic wing was designed in this paper. With the numerical calculation, it compared the aerodynamic characteristics before and after the morphing of the aircraft, and analyzed the relationship of the aircraft aerodynamic coefficient to its length, angle of attack and flight Mach number. The result showed that through morphing the movable wing, the aircraft can significantly change the lift, drag and other aerodynamic characteristics; the morphing aircraft can satisfy the dual task requirements of low-speed cruise and high-speed attack. Compared with the traditional aircraft in fixed shape, it had a better aerodynamic performance.

Original language	English
Title of host publication	Advances in Applied Science, Engineering and Technology
Pages	257-261
Number of pages	5
DOIs	https://doi.org/10.4028/www.scientific.net/AMR.709.257
Publication status	Published - 2013
Event	2013 International Conference on Applied Science, Engineering and Technology, ICASET 2013 - Qingdao, China Duration: 19 May 2013 → 21 May 2013

Publication series

Name	Advanced Materials Research
Volume	709
ISSN (Print)	1022-6680

Conference

Conference	2013 International Conference on Applied Science, Engineering and Technology, ICASET 2013
Country/Territory	China
City	Qingdao
Period	19/05/13 → 21/05/13

Keywords

Morphing aircraft
Movable wing
Telescopic wing

Access to Document

10.4028/www.scientific.net/AMR.709.257

Cite this

@inproceedings{42a19b19297642189185aa8cc4f031ea,

title = "Research on aerodynamic characteristics of morphing aircraft with a telescopic wing",

abstract = "A kind of morphing aircraft based on the concept of telescopic wing was designed in this paper. With the numerical calculation, it compared the aerodynamic characteristics before and after the morphing of the aircraft, and analyzed the relationship of the aircraft aerodynamic coefficient to its length, angle of attack and flight Mach number. The result showed that through morphing the movable wing, the aircraft can significantly change the lift, drag and other aerodynamic characteristics; the morphing aircraft can satisfy the dual task requirements of low-speed cruise and high-speed attack. Compared with the traditional aircraft in fixed shape, it had a better aerodynamic performance.",

keywords = "Morphing aircraft, Movable wing, Telescopic wing",

author = "Zhao, \{Xi You\} and Jun Hu",

year = "2013",

doi = "10.4028/www.scientific.net/AMR.709.257",

language = "English",

isbn = "9783037857182",

series = "Advanced Materials Research",

pages = "257--261",

booktitle = "Advances in Applied Science, Engineering and Technology",

note = "2013 International Conference on Applied Science, Engineering and Technology, ICASET 2013 ; Conference date: 19-05-2013 Through 21-05-2013",

}

Zhao, XY & Hu, J 2013, Research on aerodynamic characteristics of morphing aircraft with a telescopic wing. in Advances in Applied Science, Engineering and Technology. Advanced Materials Research, vol. 709, pp. 257-261, 2013 International Conference on Applied Science, Engineering and Technology, ICASET 2013, Qingdao, China, 19/05/13. https://doi.org/10.4028/www.scientific.net/AMR.709.257

TY - GEN

T1 - Research on aerodynamic characteristics of morphing aircraft with a telescopic wing

AU - Zhao, Xi You

AU - Hu, Jun

PY - 2013

Y1 - 2013

N2 - A kind of morphing aircraft based on the concept of telescopic wing was designed in this paper. With the numerical calculation, it compared the aerodynamic characteristics before and after the morphing of the aircraft, and analyzed the relationship of the aircraft aerodynamic coefficient to its length, angle of attack and flight Mach number. The result showed that through morphing the movable wing, the aircraft can significantly change the lift, drag and other aerodynamic characteristics; the morphing aircraft can satisfy the dual task requirements of low-speed cruise and high-speed attack. Compared with the traditional aircraft in fixed shape, it had a better aerodynamic performance.

AB - A kind of morphing aircraft based on the concept of telescopic wing was designed in this paper. With the numerical calculation, it compared the aerodynamic characteristics before and after the morphing of the aircraft, and analyzed the relationship of the aircraft aerodynamic coefficient to its length, angle of attack and flight Mach number. The result showed that through morphing the movable wing, the aircraft can significantly change the lift, drag and other aerodynamic characteristics; the morphing aircraft can satisfy the dual task requirements of low-speed cruise and high-speed attack. Compared with the traditional aircraft in fixed shape, it had a better aerodynamic performance.

KW - Morphing aircraft

KW - Movable wing

KW - Telescopic wing

UR - https://www.scopus.com/pages/publications/84880175703

U2 - 10.4028/www.scientific.net/AMR.709.257

DO - 10.4028/www.scientific.net/AMR.709.257

M3 - Conference contribution

AN - SCOPUS:84880175703

SN - 9783037857182

T3 - Advanced Materials Research

SP - 257

EP - 261

BT - Advances in Applied Science, Engineering and Technology

T2 - 2013 International Conference on Applied Science, Engineering and Technology, ICASET 2013

Y2 - 19 May 2013 through 21 May 2013

ER -

Research on aerodynamic characteristics of morphing aircraft with a telescopic wing

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Keywords

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