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Propulsion System Flow Stability Program (Dynamic). Part XVII. Propulsion System Simulation Digital Computer Program Format and Routines.


AD859282

Publication Date 1968
Personal Author Kaplan, E. H.; Wong, H. W.
Page Count 133
Abstract The object of the study was to develop a simulation program to be used for the evaluation of two control systems capable of sensing and accommodating a transient condition. (Author)
Keywords
  • Turbojet engines
  • Control systems
  • Models(Simulations)
  • Computer programs
  • Transients
  • Duct inlets
  • Supersonic characteristics
  • Turbofan engines
  • Flow charting
  • Subroutines
  • Digital computers
  • Input output devices
  • Computerized simulation
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 81D - Jet & Gas Turbine Engines
Corporate Authors North American Rockwell Corp Los Angeles Calif Los Angeles Div
Supplemental Notes See also Part 16, AD-852 757.
Document Type Technical Report
Title Note Final technical rept. Jun 67-Sep 68 on Phase 1.
NTIS Issue Number 197626
Contract Number
  • F33615-67-C-1848
Propulsion System Flow Stability Program (Dynamic). Part XVII. Propulsion System Simulation Digital Computer Program Format and Routines.
Propulsion System Flow Stability Program (Dynamic). Part XVII. Propulsion System Simulation Digital Computer Program Format and Routines.
AD859282

  • Turbojet engines
  • Control systems
  • Models(Simulations)
  • Computer programs
  • Transients
  • Duct inlets
  • Supersonic characteristics
  • Turbofan engines
  • Flow charting
  • Subroutines
  • Digital computers
  • Input output devices
  • Computerized simulation
  • Non Paid Delimited ADS
  • 81D - Jet & Gas Turbine Engines
  • F33615-67-C-1848
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