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PASS: A computer program for Preliminary Aircraft Structural SynthesisA computer code for Preliminary Aircraft Structural Synthesis provides rapid and accurate analysis for aircraft structures that can be adequately modeled by beam finite elements. The philosophy used in developing the program was to provide a basic framework that can be used for structural synthesis. It is anticipated that a user will need to add detail to this framework in order to perform his specific task. With this philosophy in mind, the program was written so that it is easily divided into segments, thereby making it readily adaptable. The theoretical portion of this manual describes the basic structure of the program and details the development of the unique beam element that is used. The present capability of the algorithm is stated and suggestions are made regarding enhancements to this capability. User information is also given that provides an overview of the program's construction, identifies the required inputs, describes the program output, provides some comments on the program use, and exhibits results for a simple example.
Document ID
19770020162
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnson, E. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-6954
NASA-TM-73216
Report Number: A-6954
Report Number: NASA-TM-73216
Accession Number
77N27106
Funding Number(s)
PROJECT: RTOP 505-06-19
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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