Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
Published: 1963
Total Pages: 792
ISBN-13:
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Author: United States. Superintendent of Documents
Publisher:
Published: 1963
Total Pages: 792
ISBN-13:
DOWNLOAD EBOOKAuthor: Donald M. Kuehn
Publisher:
Published: 1961
Total Pages: 32
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1962
Total Pages: 962
ISBN-13:
DOWNLOAD EBOOKAuthor: Royal Aeronautical Society
Publisher:
Published: 1962
Total Pages: 1164
ISBN-13:
DOWNLOAD EBOOKAuthor: Society of Automotive Engineers. Committee AC-9, Aircraft Environmental Systems
Publisher:
Published: 1969
Total Pages: 778
ISBN-13:
DOWNLOAD EBOOKAuthor: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher:
Published: 1961
Total Pages: 516
ISBN-13:
DOWNLOAD EBOOKAuthor: Josef Rom
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 408
ISBN-13: 1461228247
DOWNLOAD EBOOKThe 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.
Author: Holger Babinsky
Publisher: Cambridge University Press
Published: 2011-09-12
Total Pages: 481
ISBN-13: 1139498649
DOWNLOAD EBOOKShock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Author: Paul K. Chang
Publisher: Elsevier
Published: 2014-06-28
Total Pages: 800
ISBN-13: 1483181286
DOWNLOAD EBOOKInterdisciplinary and Advanced Topics in Science and Engineering, Volume 3: Separation of Flow presents the problem of the separation of fluid flow. This book provides information covering the fields of basic physical processes, analyses, and experiments concerning flow separation. Organized into 12 chapters, this volume begins with an overview of the flow separation on the body surface as discusses in various classical examples. This text then examines the analytical and experimental results of the laminar boundary layer of steady, two-dimensional flows in the subsonic speed range. Other chapters consider the study of flow separation on the two-dimensional body, flow separation on three-dimensional body shape and particularly on bodies of revolution. This book discusses as well the analytical solutions of the unsteady flow separation. The final chapter deals with the purpose of separation flow control to raise efficiency or to enhance the performance of vehicles and fluid machineries involving various engineering applications. This book is a valuable resource for engineers.