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

Item

Title
Propulsion System Flow Stability Program (Dynamic). Part XVII. Propulsion System Simulation Digital Computer Program Format and Routines
Date
1968
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFAPL TR 68-142 Part XVII
Creator
Kaplan, Earl H.
Wong, Heeman W.
Corporate Author
North American Rockwell Corp Los Angeles CA Los Angeles Div
Extent
137
NTRL Accession Number
AD859282
Identifier
AD0859282
AD0859282
Distribution Classification
1
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
AFAPL LTR
Date Modified
Scanned by request 1/14/2019 submitted by a Private Citizen (Private Citizen - No Known Affiliation)
Report Availability
Full text available
Date Issued
1968-12
Abstract
The primary objective of Task 7 of the "Propulsion System Flow Stability Program" was to develop a simulation program to be used in Phase II for the evaluation of two control systems capable of sensing and accommodating a transient condition. Since the work on this task was being performed by three companies, every effort was made to insure compatibility in terminology, units, and program documentation as well as to provide means of communicating the myriad details involved in making computer runs of the system. This documentation format is described in Section II of this volume. An early element of this task was the selection of a simulation language for use in programming the simulation. The choice of IBM's DSL/90 and the factors involved in making that choice are discussed in Section III. Simulation programs have a natural tendency to be rather voluminous and, when the system being simulated is as complex as a supersonic inlet, turbofan, and an integrated control system can be, computer storage space is rapidly filled. To alleviate this crowding, numerous logic blocks which were repetitive, such as compressor logic, were removed from the simulation logic deck and made into subroutines or functions. These subprograms are discussed in Section IV. Once the simulation logic is written, the most difficult task of all begins. The job of initialization is usually not given proper emphasis until many hours of work have convinced all concerned that it is really the most important phase. Section V discusses this task and shows an example of an initialization routine.
Publisher
Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Air Force Systems Command
Laboratory
Air Force Aero Propulsion Laboratory
Contract
F33615-67-C-1848
Distribution Conflict
No
Access Rights
Export Controls
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Media
AFAPLTR68-142part17.pdf

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