High Angle of Attack Aerodynamics

Subsonic, Transonic, and Supersonic Flows

Authors: Rom, Josef

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  • ISBN 978-1-4612-2824-0
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Softcover $99.00 net
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About this book

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.

Table of contents (1 chapter)

  • Solutions of the Navier-Stokes Equations for Flows over Configurations at High Angles of Attack

    Josef Rom

    Pages 315-384

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Buy this book

eBook $69.95 net
( price for USA )
  • ISBN 978-1-4612-2824-0
  • digitally watermarked, no DRM
  • included format: PDF
  • eBooks can be used on all Reading Devices
Softcover $99.00 net
( price for USA )
  • ISBN 978-1-4612-7686-9
  • free shipping for individuals worldwide
  • usually dispatched within 3 to 5 business days

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Bibliographic Information

Bibliographic Information
Book Title
High Angle of Attack Aerodynamics
Book Subtitle
Subsonic, Transonic, and Supersonic Flows
Copyright
1992
Publisher
Springer-Verlag New York
Copyright Holder
Springer-Verlag New York, Inc.
eBook ISBN
978-1-4612-2824-0
DOI
10.1007/978-1-4612-2824-0
Softcover ISBN
978-1-4612-7686-9
Edition Number
1
Topics