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Primer for Finite Element Multidisciplinary Engineering Analysis - STARS (AIAA Education Series) - Softcover
Synopsis
Primer for the Finite Element Multidisciplinary Analysis Computer Program - STARS is a companion publication which includes description of several new modules in STructural Analysis RoutineS (STARS), a multidisciplinary, finite element-based, graphics oriented, linear and nonlinear analysis tool. It addresses a number of disciplines as structures, heat transfer, linear aerodynamics, computational fluid dynamics, acoustics, propulsion, controls engineering and their interactions. Each individual analysis module is general-purpose in nature and is effectively integrated to yield aeroelastic and aeroservoelastic solutions to complex engineering problems. Examples of advanced NASA Dryden Flight Research Center projects analyzed by the code in recent years include the X-29A, F-18 High Alpha Research Vehicle, Hyper-X/X-43, and SOFIA (Stratospheric Observatory for Infrared Astronomy). Extensive graphics capabilities exist for convenient model development and post-processing of analysis results. The program is written in modular form in standard FORTRAN language to run on Microsoft Windows-based PCs. It provides a brief summary of theoretical formulation and solution flow charts, detailed systems description, user's guide, various analysis runstreams, data inputs for a variety of example problems, and summaries of the solution results. The associated software, along with the input data files for a variety of test cases, will enable efficient and economical solutions to a wide range of aerospace and other practical engineering problems.
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Product Description
The Primer for the Finite Element Multidisciplinary Analysis Computer Program STARS is a companion publication that describes several new modules in STructural Analysis RoutineS (STARS), a multidisciplinary, finite element-based, graphics oriented, linear and nonlinear analysis tool. It addresses such disciplines as structures, heat transfer, linear aerodynamics, computational fluid dynamics, acoustics, propulsion, controls engineering and their interactions. Each individual analysis module is general-purpose in nature and is effectively integrated to yield aeroelastic, aeroservoelastic, and aeroacoustic solutions to complex engineering problems. Examples of advanced NASA Dryden Flight Research Center projects analyzed by the code in recent years include the X-29A, F-18 High Alpha Research Vehicle, Hyper-X/X-43, and SOFIA (Stratospheric Observatory for Infrared Astronomy). Extensive graphics capabilities exist for convenient model development and post-processing of analysis results. The program is written in modular form in standard FORTRAN language to run on the Microsoft Windows operating system. It provides a brief summary of theoretical formulation and analysis flow charts, detailed systems description, user s guide, various analysis run streams, and data inputs for a variety of example problems and their solutions. When used in conjunction with this publication the software will enable efficient and economical solutions to a wide range of aerospace and other practical engineering problems.
About the Author
Kajal K. Gupta earned his Ph.D and D.Sc. degrees at the University of London. He worked at the National Physical Laboratory, Teddington before continuing his career in the United States at the NASA Dryden Flight Research Center where he has worked in such areas as numerical modeling, simulation, and flight test vehicles including the X-29A, F-18, and Hyper-X. John L. Meek earned his M.S. at the University of California, Berkeley, and his B.E. and Ph.D. from the University of Queensland in Australia. He is professor emeritus, civil engineering, at the University of Queensland.
"About this title" may belong to another edition of this title.
- PublisherAmerican Institute of Aeronautics and Astronautics
- Publication date2013
- ISBN 10 1624101747
- ISBN 13 9781624101748
- BindingPaperback
- Number of pages396
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