Title High Angle of Attack Aerodynamics : Subsonic, Transonic, and Supersonic Flows Author(s) Rom, Josef Publication New York, NY, Springer New York, 1992. Description XIII, 399 p : online resource Abstract Note 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 ISBN,Price 9781461228240 Keyword(s) 1. Aerospace engineering 2. Aerospace Technology and Astronautics 3. ASTRONAUTICS 4. Automotive engineering 5. Classical and Continuum Physics 6. Continuum physics 7. EBOOK 8. EBOOK - SPRINGER 9. Fluid- and Aerodynamics 10. FLUIDS Item Type eBook Multi-Media Links Please Click here for eBook Circulation Data Accession#   Call# Status Issued To Return Due On Physical Location I00319     On Shelf