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The potential equation has already been solved numerically in the three - dimensional case for oblique and swept-wings However, because of the periodicity of the compressor problem, the square - root transformation used in those works is not practical here. We therefore propose a new transformation, which maps the surface of the blade into a plane and includes periodicity implicitly.
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An Analysis of Three-Dimensional Transonic Compressors (Classic Reprint)
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Paperback. Zustand: New. Print on Demand. This book explores the innovative application of computational fluid dynamics in the design and evaluation of transonic compressors, vital components in aircraft engines. It presents a novel method developed by the author to simulate the complex flow around the compressor blades, taking into account viscous effects and shock waves. The method is applied to analyze the impact of blade geometry, rotational speed, and inlet conditions on compressor performance. Through numerous numerical experiments, the author illustrates how the computational model can be used to understand the complex interactions between the flow and the blade, leading to improved compressor designs with enhanced efficiency and reduced noise. The book's findings contribute to the advancement of turbomachinery design and provide valuable insights for researchers and practitioners in the field of computational fluid dynamics. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item. Bestandsnummer des Verkäufers 9781333034214_0
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PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000. Bestandsnummer des Verkäufers LW-9781333034214
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An Analysis of ThreeDimensional Transonic Compressors Classic Reprint
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PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000. Bestandsnummer des Verkäufers LW-9781333034214
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