Examination of the Improved Model for the Unsteady Combustion Around Hypersonic Projectiles PDF Download
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Author: Akiko Matsuo
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Akiko Matsuo
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Shaye Yungster
Publisher:
ISBN:
Category : Detonation waves
Languages : en
Pages : 20
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 608
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Author:
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ISBN:
Category : Airplanes
Languages : en
Pages : 626
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Author: Kazuyoshi Takayama
Publisher: Springer Science & Business Media
ISBN: 3642468764
Category : Science
Languages : en
Pages : 337
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Book Description
Ram accelerators are among the most advanced tools for generating fluid dynamcis data in supersonic reacting systems. They require the combined action of combustion, wave systems and turbulence and are still a serious challenge for physicists and engineers. This book will serve as an introductionary textbook on ram accelerators and gives a thorough overview on research activities, performance modeling and high-pressure detonation dynamics.
Author:
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Category : Aeronautics
Languages : en
Pages : 980
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Author: American Institute of Aeronautics and Astronautics. Technical Information Service
Publisher:
ISBN:
Category : AIAA paper
Languages : en
Pages : 184
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Author: Michel Roger Kamel
Publisher:
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Category :
Languages : en
Pages : 320
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Author: Akiko Matsuo
Publisher:
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Category :
Languages : en
Pages :
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722070588
Category :
Languages : en
Pages : 36
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Book Description
The development of an advanced dynamic model for aeroelastic hypersonic vehicles powered by air breathing engines requires an adequate engine model. This report provides a discussion of some of the more important features of supersonic combustion and their relevance to the analysis and design of supersonic ramjet engines. Of particular interest are those aspects of combustion that impact the control of the process. Furthermore, the report summarizes efforts to enhance the aeropropulsive/aeroelastic dynamic model developed at the Aerospace Research Center of Arizona State University by focusing on combustion and improved modeling of this flow. The expanded supersonic combustor model described here has the capability to model the effects of friction, area change, and mass addition, in addition to the heat addition process. A comparison is made of the results from four cases: (1) heat addition only; (2) heat addition plus friction; (3) heat addition, friction, and area reduction, and (4) heat addition, friction, area reduction, and mass addition. The relative impact of these effects on the Mach number, static temperature, and static pressure distributions within the combustor are then shown. Finally, the effects of frozen versus equilibrium flow conditions within the exhaust plume is discussed. Bossard, J. A. and Peck, R. E. and Schmidt, D. K. Unspecified Center NAG1-1341...
