Adaptation of SAP IV Computer Code to Aircraft Shelter Analysis Program

Abstract

This report is concerned with the adaptation of a linear, static and dynamic structural analysis computer code (SAP IV) to aircraft shelter structural components. A number of features were added to the documented version of SAP IV to decrease the time and effort necessary to set up practical problems. The Free Format Input Program enables the user to input data without the confusing and restrictive format rules of the original version. To aid in finding errors in element layout, a versatile mesh plot package has been included. A stress/displacement versus time plot capability now enables the user to generate report quality output time histories. A specific procedure for approximating the nonlinear behavior of cracked concrete has been developed and is included in this report. Although SAP IV is designed to treat a large number of different types of elements, this study was directed specifically at three element types; thin shell or plate, thick shell or plate, and beam. These elements were considered as most applicable to the aircraft shelter problem. The FFIP and mesh plotting routines are applicable only to these three elements, while the time-history plotting capability will function with all the elements presently in SAP IV.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1976
Accession Number
ADA046970

Entities

People

  • Howard L. Schreyer
  • Jerry W. Berglund
  • Joe Mccharen

Organizations

  • University of New Mexico

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Bending Moments
  • Civil Engineering
  • Computer Programs
  • Concrete
  • Dynamic Response
  • Engineering
  • Finite Element Analysis
  • Materials
  • New Mexico
  • Plastic Explosives
  • Research Facilities
  • Structural Analysis
  • Three Dimensional
  • United States

Readers

  • Computer Science.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Structural Dynamics.