High Angle of Attack Aerodynamics | Subsonic, Transonic, and Supersonic Flows

Josef Rom

ISBN 10: 1461276861 / ISBN 13: 9781461276869

Published by Springer, 2011

About this Item

High Angle of Attack Aerodynamics | Subsonic, Transonic, and Supersonic Flows | Josef Rom | Taschenbuch | xiii | Englisch | 2011 | Springer | EAN 9781461276869 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.

Seller Inventory # 106364533

Bibliographic Details

• Title: High Angle of Attack Aerodynamics | Subsonic, Transonic, and Supersonic Flows
• Publisher: Springer
• Publication Date: 2011
• Language: English
• ISBN 10: 1461276861
• ISBN 13: 9781461276869
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 235W x 155H x 23D millimeters 235 millimeters width by 155 millimeters height by 23 millimeters depth
• Weight: 628 grams
• Seller catalogs:
  • Bücher

About this title

Synopsis

The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.