This paper adapted and extended the preliminary two-step wave rotor design method with another step of experimental validation so that it became a self-validating wave rotor design method with three steps. First, the analytic design based on unsteady pressure wave models was elucidated and adapted to a design function. It was quick and convenient for a first prediction of the wave rotor. Second, the computational fluid dynamics (CFD) simulation was adapted so that it helped to adjust the first prediction. It provided detailed information of the wave rotor inner flow. Thirdly, an experimental method was proposed to complement the validation of the wave rotor design. This experimental method realized tracing the pressure waves and the flows in the wave rotor with measurement on pressure and temperature distributions. The critical point of the experiment is that the essential flow characteristics in the rotor were reflected by the measurements in the static ports. In all, the three steps compensated for each other in a global design procedure, and formed an applicable design method for generic cases.
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November 2018
Research-Article
Wave Rotor Design Method With Three Steps Including Experimental Validation
Shining Chan,
Shining Chan
School of Aerospace Engineering,
Xiamen University,
No. 422, Siming South Road, Siming District,
Xiamen 361005, Fujian, China
e-mail: chansn2007@163.com
Xiamen University,
No. 422, Siming South Road, Siming District,
Xiamen 361005, Fujian, China
e-mail: chansn2007@163.com
Search for other works by this author on:
Huoxing Liu,
Huoxing Liu
Professor
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
School of Energy and Power Engineering,
Beihang University,
XueYuan Road, No. 37, Haidian District,
Beijing 100191, China
e-mail: liuhuoxing@126.com
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
School of Energy and Power Engineering,
Beihang University,
XueYuan Road, No. 37, Haidian District,
Beijing 100191, China
e-mail: liuhuoxing@126.com
Search for other works by this author on:
Fei Xing,
Fei Xing
School of Aerospace Engineering,
Xiamen University,
Xiamen 361005, Fujian, China
e-mail: fei_xing_xmu@163.com
Xiamen University,
No. 422, Siming South Road, Siming District
,Xiamen 361005, Fujian, China
e-mail: fei_xing_xmu@163.com
Search for other works by this author on:
Hang Song
Hang Song
AVIC CAPDI Integration Equipment Co., Ltd,
Beijing 102206, China
e-mail: songhang@buaa.edu.cn
No. 2 Gaoxin 3rd Street, Changping District
,Beijing 102206, China
e-mail: songhang@buaa.edu.cn
Search for other works by this author on:
Shining Chan
School of Aerospace Engineering,
Xiamen University,
No. 422, Siming South Road, Siming District,
Xiamen 361005, Fujian, China
e-mail: chansn2007@163.com
Xiamen University,
No. 422, Siming South Road, Siming District,
Xiamen 361005, Fujian, China
e-mail: chansn2007@163.com
Huoxing Liu
Professor
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
School of Energy and Power Engineering,
Beihang University,
XueYuan Road, No. 37, Haidian District,
Beijing 100191, China
e-mail: liuhuoxing@126.com
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
School of Energy and Power Engineering,
Beihang University,
XueYuan Road, No. 37, Haidian District,
Beijing 100191, China
e-mail: liuhuoxing@126.com
Fei Xing
School of Aerospace Engineering,
Xiamen University,
Xiamen 361005, Fujian, China
e-mail: fei_xing_xmu@163.com
Xiamen University,
No. 422, Siming South Road, Siming District
,Xiamen 361005, Fujian, China
e-mail: fei_xing_xmu@163.com
Hang Song
AVIC CAPDI Integration Equipment Co., Ltd,
Beijing 102206, China
e-mail: songhang@buaa.edu.cn
No. 2 Gaoxin 3rd Street, Changping District
,Beijing 102206, China
e-mail: songhang@buaa.edu.cn
1Corresponding author.
Contributed by the Aircraft Engine Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received August 17, 2017; final manuscript received November 14, 2017; published online July 13, 2018. Assoc. Editor: Haixin Chen.
J. Eng. Gas Turbines Power. Nov 2018, 140(11): 111201 (13 pages)
Published Online: July 13, 2018
Article history
Received:
August 17, 2017
Revised:
November 14, 2017
Citation
Chan, S., Liu, H., Xing, F., and Song, H. (July 13, 2018). "Wave Rotor Design Method With Three Steps Including Experimental Validation." ASME. J. Eng. Gas Turbines Power. November 2018; 140(11): 111201. https://doi.org/10.1115/1.4038815
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