Techniques were developed and demonstrated for digital computer simulation of aircraft missions using turbo-propulsion systems. Flexible models comprised of aircraft characteristics, engine characteristics and mission profile controls are presented in detail. These models provide the capability for digital simulation of most of the practical missions conceived for singed aircraft. Instructions for and techniques of application are presented in detail. Methods for applying simulation results to mission capability analysis are discussed and examples are presented. A computer program for automatic optimization of dynamic systems is discussed along with detailed studies of its application to automatic optimization of propulsion systems to mission requirements. (Author)
Dynamic Mission Capability Analysis
1964
187 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Computer Hardware , Aeronautics , Mission profiles , Computer programs , Turbojet engines , Simulation , Digital computers , Cost effectiveness , Mach number , State-of-the-art reviews , Optimization , Aircraft , Model tests , Transients , Computer programming , Statistical analysis , Dynamic systems analyzer , Dynasar computer program , Dynasar(Dynamic systems analyzer) , Ibm 7090 , Ibm 704 , Ibm 7094 , S/L change 8404
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