PDF-(DOWNLOAD)-Low-Speed Aerodynamics (Cambridge Aerospace Series, Series Number 13)
Author : CarlyLeblanc | Published Date : 2022-09-06
Lowspeed aerodynamics is important in the design and operation of aircraft flying at low Mach number and ground and marine vehicles This text offers a modern treatment
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(DOWNLOAD)-Low-Speed Aerodynamics (Cambridge Aerospace Series, Series Number 13): Transcript
Lowspeed aerodynamics is important in the design and operation of aircraft flying at low Mach number and ground and marine vehicles This text offers a modern treatment of both the theory of inviscid incompressible and irrotational aerodynamics and the computational techniques now available to solve complex problems A unique feature is that the computational approachfrom a single vortex element to a threedimensional panel formulationis interwoven throughout This second edition features a new chapter on the laminar boundary layer emphasis on the viscousinviscid coupling the latest versions of computational techniques and additional coverage of interaction problems The authors include a systematic treatment of twodimensional panel methods and a detailed presentation of computational techniques for threedimensional and unsteady flows. 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This book includes a number of unique features to make studying computational aerodynamics more enjoyable. These include: - The computer programs used in the book\'s projects are all open source and accessible to students and practicing engineers alike on the book\'s website, www.cambridge.org/aerodynamics. The site includes access to images, movies, programs, and more - The computational aerodynamics concepts are given relevance by CA Concept Boxes integrated into the chapters to provide realistic asides to the concepts - Readers can see fluids in motion with the Flow Visualization Boxes carefully integrated into the text. This book is a modern treatment of the aerodynamic principles of helicopters and rotating-wing vertical lift aircraft. Part one covers the technical history of helicopter flight, basic methods of rotor aerodynamics, and performance-related design issues. 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