A Method For Generating Reduced Order Linear Models Of Supersonic Inlets
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Author |
: National Aeronautics and Space Administration (NASA) |
Publisher |
: Createspace Independent Publishing Platform |
Total Pages |
: 64 |
Release |
: 2018-07-02 |
ISBN-10 |
: 1722136251 |
ISBN-13 |
: 9781722136253 |
Rating |
: 4/5 (51 Downloads) |
Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by : National Aeronautics and Space Administration (NASA)
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...
Author |
: National Aeronautics and Space Adm Nasa |
Publisher |
: |
Total Pages |
: 66 |
Release |
: 2020-04-08 |
ISBN-10 |
: 1729462987 |
ISBN-13 |
: 9781729462980 |
Rating |
: 4/5 (87 Downloads) |
Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by : National Aeronautics and Space Adm Nasa
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...
Author |
: |
Publisher |
: |
Total Pages |
: 66 |
Release |
: 1997 |
ISBN-10 |
: NASA:31769000703333 |
ISBN-13 |
: |
Rating |
: 4/5 (33 Downloads) |
Synopsis A Method for Generating Reduced Order Linear Models of Supersonic Inlets by :
Author |
: |
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: |
Total Pages |
: 86 |
Release |
: 1998 |
ISBN-10 |
: NASA:31769000707367 |
ISBN-13 |
: |
Rating |
: 4/5 (67 Downloads) |
Synopsis A Method for Generating Reduced-Order Linear Models of Multidimensional Supersonic Inlets by :
Author |
: |
Publisher |
: |
Total Pages |
: 1154 |
Release |
: 1999-07 |
ISBN-10 |
: MINN:31951P007576207 |
ISBN-13 |
: |
Rating |
: 4/5 (07 Downloads) |
Synopsis Monthly Catalog of United States Government Publications by :
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: |
Publisher |
: |
Total Pages |
: 46 |
Release |
: 1998 |
ISBN-10 |
: NASA:31769000708209 |
ISBN-13 |
: |
Rating |
: 4/5 (09 Downloads) |
Synopsis To Err is Normable: The Computation of Frequency-Domain Error Bounds from Time-Domain Data by :
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: |
Publisher |
: |
Total Pages |
: 200 |
Release |
: 1997 |
ISBN-10 |
: NASA:31769000614068 |
ISBN-13 |
: |
Rating |
: 4/5 (68 Downloads) |
Synopsis Research and Technology 1996 by :
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: |
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: |
Total Pages |
: 18 |
Release |
: 1997 |
ISBN-10 |
: NASA:31769000614944 |
ISBN-13 |
: |
Rating |
: 4/5 (44 Downloads) |
Synopsis An Overview of Three Approaches to Multidisciplinary Aeropropulsion Simulations by :
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: |
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: |
Total Pages |
: 16 |
Release |
: 1994 |
ISBN-10 |
: UIUC:30112059175569 |
ISBN-13 |
: |
Rating |
: 4/5 (69 Downloads) |
Synopsis Computational Methods for HSCT-inlet Controls/CFD Interdisciplinary Research by :
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: |
Publisher |
: |
Total Pages |
: 456 |
Release |
: 1995 |
ISBN-10 |
: UIUC:30112005546491 |
ISBN-13 |
: |
Rating |
: 4/5 (91 Downloads) |
Synopsis Scientific and Technical Aerospace Reports by :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.