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    Numerical Study on the Effect of Vortex Generators on S-Shaped Intake in Propeller Slipstream 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 003:;page 04022013
    Author(s): Shuili Ren; Peiqing Liu
    Publisher: ASCE
    Abstract: In turboprop engines, the lip of the S-shaped intake is behind the propeller rotation plane, so the complex slipstream flowfield has a strong impact on the flowfield in the S-shaped intake and affects engine performance. ...
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    Detecting the Inherent Modulation Phenomenon of High-Lift Configuration Noise Using the Hilbert–Huang Transform 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 004:;page 04024039-1
    Author(s): Ling Li; Peiqing Liu
    Publisher: American Society of Civil Engineers
    Abstract: The phenomenon of multiple tones is a typical feature of high-lift configuration noise, and the underlying nonlinear and nonstationary features need to be revealed through time-frequency analysis. This paper introduces the ...
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    Effect of a Variable-Bend Slat on Tones Due to the Cove’s Self-Excited Oscillation 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 006:;page 04021077-1
    Author(s): Yuan Liu; Peiqing Liu; Hao Guo; Tianxiang Hu
    Publisher: ASCE
    Abstract: To study the noise reduction effect of a variable-bend slat, both experimental and numerical investigations are carried out on a two-dimensional high-lift configuration with a stowed flap at varying angle of attack. With ...
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    Platform for Transport Aircraft Wing–Body Parametric Modeling and High-Lift System Design 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author(s): Yun Tian; Xiangnan Qu; Peiqing Liu; Shiwei Yan
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, the authors describe a software they have developed for wing–body parametric modeling and high-lift system design. This software has the following features: (1) it generates and modifies geometric as ...
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    Gurney-Flap Drag Penalty Reduction with a DBD Plasma Actuator 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author(s): Zeng Zhang; Lihao Feng; Jinjun Wang; Peiqing Liu
    Publisher: American Society of Civil Engineers
    Abstract: The present research proposed a method to reduce the Gurney-flap drag penalty with a dielectric barrier discharge (DBD) plasma actuator, which was mounted in front of the Gurney flap to generate a countercurrent wall jet. ...
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    Experimental Investigation of the Far-Field Noise Generated from the Cruise Configuration of Aircraft High-Lift Device 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    Author(s): Ling Li; Peiqing Liu; Hao Guo; Yujia Hou
    Publisher: ASCE
    Abstract: Air traffic has developed rapidly in the last decades. The noise generated from aircraft can impair the health of passengers and airport residents, so it is necessary to reduce aircraft noise and relieve the annoyance due ...
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    Experimental Study of Far-Field Radiated Noise Characteristics for the Leading-Edge Slat of a 30P30N Airfoil 

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 006:;page 04023070-1
    Author(s): Xin Geng; Peiqing Liu; Hao Guo; Tianxiang Hu; Ling Li; Yuan Liu
    Publisher: ASCE
    Abstract: To study the far-field aerodynamic noise of the leading-edge slat of a high-lift airfoil configuration, an experimental investigation of the BANC-II/30P30N airfoil model was carried out in the D5 areo-acoustic wind tunnel ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian