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Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
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Book Description
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: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
Get Book Here
Book Description
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: Robert Godwin
Publisher: Burlington, Ont. : Apogee Books
ISBN: 9781896522951
Category : History
Languages : en
Pages : 484
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Book Description
It was a Space Shuttle with a mission - to drop a weaponpayload anywhere on Earth and to do so while approachingits target at hypersonic velocity - 18,000 miles perhour. Between 1957 and 1963 the Dyna-Soar programconsumed $430 million of the US taxpayer's money.However, it never flew. Cancelled less than two weeksafter President ......
Author: John J. Bertin
Publisher: AIAA
ISBN: 9781563470363
Category : Science
Languages : en
Pages : 644
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Book Description
A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer. Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design considerations. Includes sample exercises and homework problems. Annotation copyright by Book News, Inc., Portland, OR
Author: Frank K. Lu
Publisher: AIAA
ISBN: 9781600864483
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 694
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Book Description
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309061423
Category : Technology & Engineering
Languages : en
Pages : 76
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Book Description
This study was undertaken in response to a request by the U.S. Air Force that the National Research Council (NRC) examine whether the technologies that underlie the concept of a hypersonic, air-launched, air-breathing, hydrocarbon-fueled missile with speeds up to Mach 81 can be demonstrated in time to be initially operational by 2015. To conduct the study, the NRC appointed the Committee on Review and Evaluation of the Air Force Hypersonic Technology Program, under the auspices of the Air Force Science and Technology Board.
Author: William H. Heiser
Publisher: AIAA
ISBN: 9781563470356
Category : Science
Languages : en
Pages : 632
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Book Description
An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR
Author: Dennis R. Jenkins
Publisher:
ISBN: 9781580071314
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
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Book Description
Nineteen years before Space Shuttle, the small, black, rocket-powered, bullet-shaped X-15 showed it was possible to fly into - and out of - space. There had never been anything like the X-15; it had a million-horsepower engine and could fly twice as fast as a rifle bullet. The X-15 set records that stood for years. Specialty Press's bestseller, Hypersonic, has been re-released in a softbound format at a reduced price. This book is the most extensively researched history of the X-15 program yet published. The book was written with the cooperation of surviving X-15 pilots as well as many other program principals and is based on six years of research in Air Force, NASA, and North American archives. It covers the tasks of converting and testing the B-52 carrier airplanes, building the first full-pressure suits to protect the pilot, building the first engineering mission simulators, acquiring the remote lakebed landing sites, and building the radar range. It also covers the flight program in detail, including the most authoritative flight log ever assembled; in many instances, information in this log was derived from the original flight-data recordings. Also covered are each of the experiments that were flown aboard the X-15 late in its career when it became the workhorse of the space program, carrying such things as startrackers destined for the Apollo program and missile-detection systems that would later be sent into orbit on satellites.
Author: Maurice Rasmussen
Publisher: Wiley-Interscience
ISBN: 9780471511021
Category : Technology & Engineering
Languages : en
Pages : 0
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Book Description
The Ideal Text/Reference for Students, Engineers, and Research Scientists Not since the early days of space flight has the subject of hypersonic flow been of such importance to aerospace and mechanical engineers, research scientists, and students. Spurred by visions of hypersonic transport, and aerospace planes, the government now supports studies of hypersonic flow in at least eighteen graduate research centers across the nation, and numerous major universities now offer graduate and senior level undergraduate courses on the subject. Hypersonic Flow is the ideal text/reference for students and professionals interested in this burgeoning field. Written by a nationally recognized authority on the subject, it features a clear, accessible writing style along with sufficient depth and detail for self-study, and it is organized for speedy location of specific information. Numerous end-of-chapter exercises and homework problems enhance and solidify the student’s understanding of complex and sophisticated material. This book provides an in-depth look at all the major topics and issues associated with fluid flow at speeds in excess of Mach 5, including: elementary hypersonic flow problems; general similarity concepts; elements of hypersonic small disturbance theory; and much more. In addition, this book brings you: The most extensive coverage of viscous effects available anywhere A unique, in-depth presentation of waveriders Extensive treatment of asymmetric conical flows An introduction to computational fluid dynamics Extensive treatment of real-gas effects
Author: Joseph J.S. Shang
Publisher: CRC Press
ISBN: 1000876993
Category : Science
Languages : en
Pages : 327
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Book Description
Classic and High-Enthalpy Hypersonic Flows presents a complete look at high-enthalpy hypersonic flow from a review of classic theories to a discussion of future advances centering around the Born-Oppenheim approximation, potential energy surface, and critical point for transition. The state-of-the-art hypersonic flows are defined by a seamless integration of the classic gas dynamic kinetics with nonequilibrium chemical kinetics, quantum transitions, and radiative heat transfer. The book is intended for graduate students studying advanced aerodynamics and taking courses in hypersonic flow. It can also serve as a professional reference for practicing aerospace and mechanical engineers of high-speed aerospace vehicles and propulsion system research, design, and evaluation. Features Presents a comprehensive review of classic hypersonic flow from the Newtonian theory to blast wave analogue. Introduces nonequilibrium chemical kinetics to gas dynamics for hypersonic flows in the high-enthalpy state. Integrates quantum mechanics to high-enthalpy hypersonic flows including dissociation and ionization. Covers the complete heat transfer process with radiative energy transfer for thermal protection of earth reentry vehicle. Develops and verifies the interdisciplinary governing equations for understanding and analyzing realistic hypersonic flows.
Author: Wilbur C. Nelson
Publisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
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Book Description
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
