17th Joint Propulsion Conference 1981
DOI: 10.2514/6.1981-1362
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Effect of a part-span variable inlet guide vane on the performance of a high-bypass turbofan engine

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“…3,10 VIGVs are also used widely in Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China fans of conventional turbo-engines for adjusting their working lines. 11,12 M Boehle et al 13 compared the flow fields of VIGVs with that of invariable inlet guide vanes (IIGVs) and determined that the VIGVs had a favorable pressure distribution on the vane surfaces in comparison with the IIGVs and that the flow losses of the VIGVs were lower than those of the IIGVs. C Celis et al 14 proposed correction factors that can be used to modify the compressor characteristics map as a function of the VIGV angles.…”
Section: Introductionmentioning
confidence: 99%
“…3,10 VIGVs are also used widely in Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China fans of conventional turbo-engines for adjusting their working lines. 11,12 M Boehle et al 13 compared the flow fields of VIGVs with that of invariable inlet guide vanes (IIGVs) and determined that the VIGVs had a favorable pressure distribution on the vane surfaces in comparison with the IIGVs and that the flow losses of the VIGVs were lower than those of the IIGVs. C Celis et al 14 proposed correction factors that can be used to modify the compressor characteristics map as a function of the VIGV angles.…”
Section: Introductionmentioning
confidence: 99%