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A Method For Generating Reduced Order Linear Models Of Multidimensional Supersonic Inlets
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Book Synopsis A Method for Generating Reduced-Order Linear Models of Multidimensional Supersonic Inlets by :
Download or read book A Method for Generating Reduced-Order Linear Models of Multidimensional Supersonic Inlets written by and published by . This book was released on 1998 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by :
Download or read book A Method for Generating Reduced Order Linear Models of Supersonic Inlets written by and published by . This book was released on 1997 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Methods for HSCT-inlet Controls/CFD Interdisciplinary Research by :
Download or read book Computational Methods for HSCT-inlet Controls/CFD Interdisciplinary Research written by and published by . This book was released on 1994 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference by :
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722136253 Total Pages :64 pages Book Rating :4.1/5 (362 download)
Book Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by : National Aeronautics and Space Administration (NASA)
Download or read book A Method for Generating Reduced Order Linear Models of Supersonic Inlets written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: For the modeling of high speed propulsion systems, there are at least two major categories of models. One is based on computational fluid dynamics (CFD), and the other is based on design and analysis of control systems. CFD is accurate and gives a complete view of the internal flow field, but it typically has many states and runs much slower dm real-time. Models based on control design typically run near real-time but do not always capture the fundamental dynamics. To provide improved control models, methods are needed that are based on CFD techniques but yield models that are small enough for control analysis and design. Chicatelli, Amy and Hartley, Tom T. Glenn Research Center...
Book Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by : National Aeronautics and Space Adm Nasa
Download or read book A Method for Generating Reduced Order Linear Models of Supersonic Inlets written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2020-04-08 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: For the modeling of high speed propulsion systems, there are at least two major categories of models. One is based on computational fluid dynamics (CFD), and the other is based on design and analysis of control systems. CFD is accurate and gives a complete view of the internal flow field, but it typically has many states and runs much slower dm real-time. Models based on control design typically run near real-time but do not always capture the fundamental dynamics. To provide improved control models, methods are needed that are based on CFD techniques but yield models that are small enough for control analysis and design. Chicatelli, Amy and Hartley, Tom T. Glenn Research Center...
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