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Title
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Propulsion System Flow Stability Program (Dynamic). Part XX. Computer Programs for the Root Locus Analysis of Linearized Turbojet and Turbofan Control Systems
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Date
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1968
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Index Abstract
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Coming Soon
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Photo Quality
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Not Needed
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Report Number
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AFAPL TR 68-142 Part XX
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Creator
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Lum, Evan L.
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Corporate Author
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North American Rockwell Corp Los Angeles CA Los Angeles Div
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Extent
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95
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NTRL Accession Number
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AD853262
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Identifier
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AD0853262
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AD0853262
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Distribution Classification
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1
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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None
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Date Modified
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Scanned by request 1/15/2019 submitted by a Private Citizen (Private Citizen - No Known Affiliation)
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Report Availability
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Full text available
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Date Issued
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1968-12
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Abstract
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This part describes computer programs developed to handle the computational tasks for the linear stability analysis of propulsion controls by root locus techniques. The descriptions, flowcharts, and Fortran program listings of two main programs TJET and TFAN developed for the analysis of turbojet and turbofan engine control systems are presented. Also presented are the descriptions of three subroutines specially developed to facilitate data handling for this study. Examples are given to illustrate the application of computer programs TJET and TFAN. TJET and TFAN have been valuable in the linear analysis of the propulsion system, However, it is recommended that these computer programs be expanded to include the capability of analyzing coupled control loops and to include a limited transient analysis.
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Publisher
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Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Air Force Systems Command
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Laboratory
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Air Force Aero Propulsion Laboratory
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Contract
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F33615-67-C-1848
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Distribution Conflict
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No
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Access Rights
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Export Controls
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource
AFAPLTR68-142part20.pdf