Monthly Catalog of United States Government Publications
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1812 |
Release | : 1960 |
Genre | : Government publications |
ISBN | : |
Download Effect Of Slight Blunting Of Leading Edge Of Immersed Body On Flow Around It At Hypersonic Speeds With List Of Literature Cited full books in PDF, epub, and Kindle. Read online free Effect Of Slight Blunting Of Leading Edge Of Immersed Body On Flow Around It At Hypersonic Speeds With List Of Literature Cited ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1812 |
Release | : 1960 |
Genre | : Government publications |
ISBN | : |
Author | : John David Anderson |
Publisher | : AIAA |
Total Pages | : 710 |
Release | : 1989 |
Genre | : Science |
ISBN | : 9781563474590 |
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author | : T.A. Heppenheimer |
Publisher | : Courier Dover Publications |
Total Pages | : 355 |
Release | : 2018-09-12 |
Genre | : Technology & Engineering |
ISBN | : 0486834514 |
This volume from The NASA History Series presents an overview of the science of hypersonics, the study of flight at speeds at which the physics of flows is dominated by aerodynamic heating. The survey begins during the years immediately following World War II, with the first steps in hypersonic research: the development of missile nose cones and the X-15; the earliest concepts of hypersonic propulsion; and the origin of the scramjet engine. Next, it addresses the re-entry problem, which came to the forefront during the mid-1950s, showing how work in this area supported the manned space program and contributed to the development of the orbital shuttle. Subsequent chapters explore the fading of scramjet studies and the rise of the National Aerospace Plane (NASP) program of 1985–95, which sought to lay groundwork for single-stage vehicles. The program's ultimate shortcomings — in terms of aerodynamics, propulsion, and materials — are discussed, and the book concludes with a look at hypersonics in the post-NASP era, including the development of the X-33 and X-34 launch vehicles, further uses for scramjets, and advances in fluid mechanics. Clearly, ongoing research in hypersonics has yet to reach its full potential, and readers with an interest in aeronautics and astronautics will find this book a fascinating exploration of the field's history and future.
Author | : Holt Ashley |
Publisher | : Courier Corporation |
Total Pages | : 306 |
Release | : 1965-01-01 |
Genre | : Technology & Engineering |
ISBN | : 0486648990 |
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
Author | : Alvin Seiff |
Publisher | : |
Total Pages | : 28 |
Release | : 1962 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : Josef Rom |
Publisher | : Springer Science & Business Media |
Total Pages | : 408 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 1461228247 |
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.
Author | : Wallace Hayes |
Publisher | : Elsevier |
Total Pages | : 481 |
Release | : 2012-12-02 |
Genre | : Technology & Engineering |
ISBN | : 032314876X |
Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.
Author | : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md |
Publisher | : |
Total Pages | : 516 |
Release | : 1961 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Author | : Luigi Crocco |
Publisher | : |
Total Pages | : 236 |
Release | : 1946 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.