A Method for Generating Reduced Order Linear Models of Supersonic Inlets

A Method for Generating Reduced Order Linear Models of Supersonic Inlets
Author :
Publisher : Createspace Independent Publishing Platform
Total Pages : 64
Release :
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...

A Method for Generating Reduced Order Linear Models of Supersonic Inlets

A Method for Generating Reduced Order Linear Models of Supersonic Inlets
Author :
Publisher :
Total Pages : 66
Release :
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...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author :
Publisher :
Total Pages : 456
Release :
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.