Proceedings of the Conference on Matrix Methods in Structural Mechanics (2nd) Held At Wright Patterson Air Force Base, Ohio, On 1517 October 1968
Report Number: AFFDL TR 68150
Corporate Author: Air Force Flight Dynamics Lab WrightPatterson AFB Ohio
Date of Publication: 196912
Pages: 1462
AD Number: AD0703685
Provenance:
Lockheed Martin Missiles & Fire Control
Corporate Author: Air Force Flight Dynamics Lab WrightPatterson AFB Ohio
Date of Publication: 196912
Pages: 1462
AD Number: AD0703685
Abstract:
The purpose of the conference was to discuss the recent developments in matrix structural analysis and design of structural systems. Forty papers were presented in seven sessions entitled: Structural weight Optimization; Dynamics; General Elements; Curved Elements; Applications; General Methods; and Nonlinear Analysis.
The purpose of the conference was to discuss the recent developments in matrix structural analysis and design of structural systems. Forty papers were presented in seven sessions entitled: Structural weight Optimization; Dynamics; General Elements; Curved Elements; Applications; General Methods; and Nonlinear Analysis.
Provenance:
Lockheed Martin Missiles & Fire Control
Conference papers and presentations are scanned individually
See individual reports below to check for availability
See individual reports below to check for availability
Other options for obtaining this report
Via the Defense Technical Information Center (DTIC):A record for this report, and possibly a fullimage download of the report, exists at DTIC
Via National Technical Information Service:
This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library
Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Related Reports
This conference contains the following reports:

Table of Contents
AFFDL TR 68150 p. iix 
Addresses
AFFDL TR 68150 p. 113 
Matrix Methods of Aerospace Structural Analysis
AFFDL TR 68150 p. 1579 
Application of the Created Response Surface Technique to Structural Optimization
AFFDL TR 68150 p. 83110 
Optimization of Structures Based on the Study of Energy Distribution
AFFDL TR 68150 p. 111153 
FullyStressed Design of Airplane Redundant Structures
AFFDL TR 68150 p. 155181 
Dynamic Analysis of Shells Using DoubleCurved Finite Elements
AFFDL TR 68150 p. 185212 
Static and Dynamic Finite Element Analysis of Sandwich Structures
AFFDL TR 68150 p. 213245 
Vibration Analysis of Cantilevered Curved Plates Using a New Cylindrical Shell Finite Element
AFFDL TR 68150 p. 247269 
A Minimization Method for the Solution of the Eigenproblem Arising in Structural Dynamics
AFFDL TR 68150 p. 271306 
A Practical Computational Method for Reducing a Dynamical System with Constraints to an Equivalent System with Independent Coordinates
AFFDL TR 68150 p. 307330 
Some New Elements for the Matrix Displacement Method
AFFDL TR 68150 p. 333397 
A Refined Quadrilateral Element for Analysis of Plate Bending
AFFDL TR 68150 p. 399440 
Rationalization in Deriving Element Stiffness Matrix by Assumed Stress Approach
AFFDL TR 68150 p. 441469 
A Finite Element Application of the HellingerReissner Variational Theorem
AFFDL TR 68150 p. 471487 
Finite Elements in Linear Viscoelasticity
AFFDL TR 68150 p. 489516 
Finite Element Analysis of Fluid Flows
AFFDL TR 68150 p. 517535 
Curved Thick Shell and Membrane Elements with Particular Reference to Axisymmetric Problems
AFFDL TR 68150 p. 539572 
Finite Element Analysis of Sandwich Plates and Cylindrical Shells with Laminated Faces
AFFDL TR 68150 p. 573616 
Curved Triangular Elements for the Analysis of Shells
AFFDL TR 68150 p. 617639 
A Doubly Curved Triangular Shell Element
AFFDL TR 68150 p. 641666 
The Analysis of Thin Shells with Transverse Shear Strains by the Finite Element Method
AFFDL TR 68150 p. 667710 
Elastic Instability Predictions for DoublyCurved Shells
AFFDL TR 68150 p. 711739 
Analysis of the 747 Aircraft WingBody Intersection
AFFDL TR 68150 p. 743788 
Structural Analysis Practices for Large Scale Systems
AFFDL TR 68150 p. 789838 
Applications Experience with the Format Computer Program
AFFDL TR 68150 p. 839867 
Some Applications of Finite Analysis to Shell Buckling Prediction
AFFDL TR 68150 p. 869893 
Structural Survivability Analysis
AFFDL TR 68150 p. 895928 
The Role of Computer Graphics in the Structural Design Process
AFFDL TR 68150 p. 929964 
A Method for the Complicated Buckling Problems of Elastic Plates with Combined Use of RayleighRitz's Procedure in the Finite Element Method
AFFDL TR 68150 p. 967994 
Accuracy and Convergence of Finite Element Approximations
AFFDL TR 68150 p. 9951027 
Numerical Conditioning of Stiffness Matrix Formulations for Frame Structures
AFFDL TR 68150 p. 10291060 
Completeness and Convergence in the Finite Element Method
AFFDL TR 68150 p. 10611089 
Analysis of General Coupled Thermoelasticity Problems by the Finite Element Method
AFFDL TR 68150 p. 10911120 
The Heat Conduction and Thermal Stress Analysis by the Finite Element Method
AFFDL TR 68150 p. 11211163 
Hydroelastic of Axisymmetric Systems by a Finite Element Method
AFFDL TR 68150 p. 11651203 
An Approximate Analysis of Thin Plates
AFFDL TR 68150 p. 12071230 
Linear and Nonlinear Analysis of Shells of Revolution with Asymmetrical Stiffness Properties
AFFDL TR 68150 p. 12311251 
Analysis of Tension Structures
AFFDL TR 68150 p. 12531270 
Analysis of the ElasticPlastic Problems by the Matrix Displacement Method
AFFDL TR 68150 p. 12711299 
A Finite Element Method for the Plastic Bending Analysis of Structures
AFFDL TR 68150 p. 13011339 
Progress Report on DiscreteElement Elastic and ElasticPlastic Analyses of Shells of Revolution Subjected to Axisymmetric and Asymmetric Loading
AFFDL TR 68150 p. 13411453