Author: Great Britain. Royal Commission on Scientific Instruction and the Advancement of Science
Publisher:
ISBN:
Category : Cultural policy
Languages : en
Pages : 590
Book Description
Progress in Aeronautical Sciences
Author: D. Küchemann
Publisher: Elsevier
ISBN: 1483145336
Category : Technology & Engineering
Languages : en
Pages : 540
Book Description
Progress in Aeronautical Sciences, Volume 10 provides information pertinent to the development in aeronautical sciences. This book discusses a variety of topics, including thermoelasticity, turbulent boundary, as well as the manufacturing methods, reliability, problem areas, and applications under development in fluidic systems. Organized into six chapters, this volume begins with an overview of the theoretical problems of elasticity. This text then discusses the state of research in the complex fields of turbulent boundary layers with fluid injections. Other chapters consider as well the problems of supersonic flow past wings and bodies. This book discusses as well the flow in hypersonic wakes in ionized gases. The reader is also introduced to the possible applications of the compressible turbulent boundary layer with fluid injection. The final chapter discusses the components used in fluidic systems, which are described with emphasis on their general system of operation and general properties. This book is a valuable resource for engineers.
Publisher: Elsevier
ISBN: 1483145336
Category : Technology & Engineering
Languages : en
Pages : 540
Book Description
Progress in Aeronautical Sciences, Volume 10 provides information pertinent to the development in aeronautical sciences. This book discusses a variety of topics, including thermoelasticity, turbulent boundary, as well as the manufacturing methods, reliability, problem areas, and applications under development in fluidic systems. Organized into six chapters, this volume begins with an overview of the theoretical problems of elasticity. This text then discusses the state of research in the complex fields of turbulent boundary layers with fluid injections. Other chapters consider as well the problems of supersonic flow past wings and bodies. This book discusses as well the flow in hypersonic wakes in ionized gases. The reader is also introduced to the possible applications of the compressible turbulent boundary layer with fluid injection. The final chapter discusses the components used in fluidic systems, which are described with emphasis on their general system of operation and general properties. This book is a valuable resource for engineers.