Exploratory Investigation Of Aerodynamic Effects Of External Combustion Of Aluminum Borohydride In Airstream Adjacent To Flat Plate In Mach 246 Tunnel
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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 | : Air Pollution Technical Information Center |
Publisher | : |
Total Pages | : 824 |
Release | : 1971 |
Genre | : Air |
ISBN | : |
About 1900 references, intended as a balanced sample of available literature mostly from the period 1959-1970. Foreign literature is included. Entries are arranged under topics. Author, title, subject, and geographic location indexes.
Author | : Jiun-Ming Li |
Publisher | : Springer |
Total Pages | : 246 |
Release | : 2017-12-05 |
Genre | : Technology & Engineering |
ISBN | : 3319689061 |
This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE). State-of-the-art research contributions are collected from international leading researchers devoted to the pursuit of controllable detonations for practical detonation propulsion. A system-level design of novel detonation engines, performance analysis, and advanced experimental and numerical methods are covered. In addition, the world’s first successful sled demonstration of a rocket rotating detonation engine system and innovations in the development of a kilohertz pulse detonation engine (PDE) system are reported. Readers will obtain, in a straightforward manner, an understanding of the RDE & PDE design, operation and testing approaches, and further specific integration schemes for diverse applications such as rockets for space propulsion and turbojet/ramjet engines for air-breathing propulsion. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines provides, with its comprehensive coverage from fundamental detonation science to practical research engineering techniques, a wealth of information for scientists in the field of combustion and propulsion. The volume can also serve as a reference text for faculty and graduate students and interested in shock waves, combustion and propulsion.
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 | : Henry C. Barnett |
Publisher | : |
Total Pages | : 62 |
Release | : 1948 |
Genre | : Fuel |
ISBN | : |
This paper presents the results showing the antiknock performance characteristics of proposed reference fuels (triptane, n-heptane, isooctane) in current fuel knock-rating engines. The proposed reference-fuel scales are compared with the octane-number scale and the performance-number scale now in use.
Author | : J. W. McBain |
Publisher | : |
Total Pages | : 32 |
Release | : 1949 |
Genre | : Charcoal |
ISBN | : |
Lubricating oil has been processed by treatment with various adsorbaents and by solvent extraction in an attempt to reduce foaming.
Author | : J. W. McBain |
Publisher | : |
Total Pages | : 24 |
Release | : 1949 |
Genre | : Lubrication and lubricants |
ISBN | : |
The surface properties of oils were studied in a short series of experiments on their film viscosities and surface tensions. Information about film formation in general was obtained from the behavior of single bubbles on the surface and from the coalesence of pairs of bubbles below the surface of various pure and binary liquids.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 230 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : Edward A. Fletcher |
Publisher | : |
Total Pages | : 82 |
Release | : 1955 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
The feasibility of adding heat to a supersonic airstream in the absence of flameholders was studied. Transient burning for periods of 3 to 10 milliseconds was achieved in a supersonic wind tunnel at nominal Mach numbers of 1.5, 2, 3, and 4. Steady burning was achieved for periods of 0.2 to 2 seconds at nominal Mach numbers of 1.5, 2, and 3. Burning and tunnel flow phenomena, including thermal choking, are described. Possible applications of the results of this study are suggested.
Author | : |
Publisher | : |
Total Pages | : 492 |
Release | : 1977 |
Genre | : |
ISBN | : |