A novel pulsed microblowing technique to improve flow separation over flap

Y. K. Wang; P. Zhou; X. Y. Deng; Q. Li; D. J. Zhao

doi:10.1016/j.proeng.2013.12.003

A novel pulsed microblowing technique to improve flow separation over flap

Y. K. Wang^*
, P. Zhou
, X. Y. Deng
, Q. Li
, D. J. Zhao

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Conference article › peer-review

1 Scopus citations

Abstract

A new flow control technique to improve the flow separation over flap by pulsed microblowing at the flow separated position is discussed in this paper. Firstly, the effect of various blowing parameters, including average blowing momentum and pulse frequency, are investigated in detail. Secondly, based on the comparison between the effects of continuous blowing and pulsed blowing, the mechanism of pulsed blowing flow control technique is also discussed. All of the tests have been conducted at low-speed wind tunnel with Reynolds number of 0.6×10⁵-1.2×10⁶ at flap deflection angle of δ_e=20° in Beijing University of Aeronautics and Astronautics.

Original language	English
Pages (from-to)	25-49
Number of pages	25
Journal	Procedia Engineering
Volume	67
DOIs	https://doi.org/10.1016/j.proeng.2013.12.003
State	Published - 2013
Event	7th Asian-Pacific Conference on Aerospace Technology and Science, APCATS 2013 - Sun-moon Lake, Taiwan, Province of China Duration: 23 May 2013 → 26 May 2013

Keywords

Flap
Flow control
Flow separation
Pulsed blowing
Tailless aircraft

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10.1016/j.proeng.2013.12.003

Cite this

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title = "A novel pulsed microblowing technique to improve flow separation over flap",

abstract = "A new flow control technique to improve the flow separation over flap by pulsed microblowing at the flow separated position is discussed in this paper. Firstly, the effect of various blowing parameters, including average blowing momentum and pulse frequency, are investigated in detail. Secondly, based on the comparison between the effects of continuous blowing and pulsed blowing, the mechanism of pulsed blowing flow control technique is also discussed. All of the tests have been conducted at low-speed wind tunnel with Reynolds number of 0.6×105-1.2×106 at flap deflection angle of δe=20° in Beijing University of Aeronautics and Astronautics.",

keywords = "Flap, Flow control, Flow separation, Pulsed blowing, Tailless aircraft",

author = "Wang, \{Y. K.\} and P. Zhou and Deng, \{X. Y.\} and Q. Li and Zhao, \{D. J.\}",

year = "2013",

doi = "10.1016/j.proeng.2013.12.003",

language = "英语",

volume = "67",

pages = "25--49",

journal = "Procedia Engineering",

issn = "1877-7058",

publisher = "Elsevier Ltd",

note = "7th Asian-Pacific Conference on Aerospace Technology and Science, APCATS 2013 ; Conference date: 23-05-2013 Through 26-05-2013",

}

TY - JOUR

T1 - A novel pulsed microblowing technique to improve flow separation over flap

AU - Wang, Y. K.

AU - Zhou, P.

AU - Deng, X. Y.

AU - Li, Q.

AU - Zhao, D. J.

PY - 2013

Y1 - 2013

N2 - A new flow control technique to improve the flow separation over flap by pulsed microblowing at the flow separated position is discussed in this paper. Firstly, the effect of various blowing parameters, including average blowing momentum and pulse frequency, are investigated in detail. Secondly, based on the comparison between the effects of continuous blowing and pulsed blowing, the mechanism of pulsed blowing flow control technique is also discussed. All of the tests have been conducted at low-speed wind tunnel with Reynolds number of 0.6×105-1.2×106 at flap deflection angle of δe=20° in Beijing University of Aeronautics and Astronautics.

AB - A new flow control technique to improve the flow separation over flap by pulsed microblowing at the flow separated position is discussed in this paper. Firstly, the effect of various blowing parameters, including average blowing momentum and pulse frequency, are investigated in detail. Secondly, based on the comparison between the effects of continuous blowing and pulsed blowing, the mechanism of pulsed blowing flow control technique is also discussed. All of the tests have been conducted at low-speed wind tunnel with Reynolds number of 0.6×105-1.2×106 at flap deflection angle of δe=20° in Beijing University of Aeronautics and Astronautics.

KW - Flap

KW - Flow control

KW - Flow separation

KW - Pulsed blowing

KW - Tailless aircraft

UR - https://www.scopus.com/pages/publications/84893368328

U2 - 10.1016/j.proeng.2013.12.003

DO - 10.1016/j.proeng.2013.12.003

M3 - 会议文章

AN - SCOPUS:84893368328

SN - 1877-7058

VL - 67

SP - 25

EP - 49

JO - Procedia Engineering

JF - Procedia Engineering

T2 - 7th Asian-Pacific Conference on Aerospace Technology and Science, APCATS 2013

Y2 - 23 May 2013 through 26 May 2013

ER -

A novel pulsed microblowing technique to improve flow separation over flap

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Keywords

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