38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2002
DOI: 10.2514/6.2002-3536
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Approach to High Performance Transonic Centrifugal Compressor

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Cited by 9 publications
(6 citation statements)
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“…Therefore, adjusting and controlling the thickness distribution of the suction surface is the key point to improve the flow in the blade passage. Oana [8] studied the influence of the thickness distribution of rotary profile for the centrifugal compressor performance. The thickness distribution of pressure surface and suction surface has been given respectively.…”
Section: Impellermentioning
confidence: 99%
“…Therefore, adjusting and controlling the thickness distribution of the suction surface is the key point to improve the flow in the blade passage. Oana [8] studied the influence of the thickness distribution of rotary profile for the centrifugal compressor performance. The thickness distribution of pressure surface and suction surface has been given respectively.…”
Section: Impellermentioning
confidence: 99%
“…The results showed that the size and location of the splitter blades were influenced on the overall performance of the centrifugal impeller. Oana et al [4] suggested that splitter incidence angle affects positively the overall efficiency of an impeller.…”
Section: Introductionmentioning
confidence: 99%
“…He achieved enhanced blade loading distribution and efficiency. By changing blade thickness and shape, Ona et al [19] retrofitted the compressor and succeeded in reducing rapid fluid flow acceleration/deceleration at leading edge and separation phenomena at hub.…”
Section: Introductionmentioning
confidence: 99%