Electric Charge Build-up in Hypersonic Wind Tunnels with Electron Beam Energy Addition PDF Download
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Author: M. N. Shneider
Publisher:
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Category :
Languages : en
Pages :
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Author: M. N. Shneider
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1184
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 134
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Results and analysis of the RDHWT/MARlAH II 1 MW experiment are reported. The experiment is the addition of approximately MW of energy to a supersonic air flow with an electron bean. The experiment hardware, arrangement and conduct are described. Selected data and analysis are reported. The experiment was subject to transient power fluctuations flat were traced to the electron beam source rather than to flow instability. Power stability was established at lower power conditions. and these data were used for selected code validations.
Author:
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Category :
Languages : en
Pages : 4
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Author: C. C. Limbaugh
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Category :
Languages : en
Pages :
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 786
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Book Description
Author: Frank K. Lu
Publisher: AIAA
ISBN: 9781600864483
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 694
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Author: S. Macheret
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Victor R. Buonadonna
Publisher:
ISBN:
Category : Gasdynamic lasers
Languages : en
Pages : 0
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Book Description
A preliminary analytic feasibility study has been made concerning the addition of stagnation enthalpy to the air flow of a hypersonic wind tunnel by volume energy addition using a high power (megawatts) CO2 laser. A model has been formulated on the basis of quasi one-dimensional, steady flow in a Laval nozzle with a collimated laser beam propagating in the downstream direction. Stagnation conditions on the order of 10,000K at 1,000 atm. are possible with 10% head losses. Heat transfer rate at the throat (50 kWatts/square centimeter) is the major limiting factor to successful operation. (Author).
Author: T.A. Heppenheimer
Publisher: Courier Dover Publications
ISBN: 0486834514
Category : Technology & Engineering
Languages : en
Pages : 355
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Book Description
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.
