DEVELOPMENT OF THERMALLY INDUCED INITIAL DISPLACEMENT MATRICES FOR THE FUSELAGE ANALYSIS PROGRAM

In preparation for the development of thermal capabilities into the fuselage analysis program, FUSARG, the thermal displacement column or H matrix for the idealized elements of this program were developed. The elements under consideration were the: (1) composite frame, (2) longitudinal effective fla...

Full description

Saved in:
Bibliographic Details
Main Author: Carpenter,William C
Format: Report
Language:English
Subjects:
Aircraft
COMPUTER PROGRAMMING
DEFORMATION
FUSELAGES
LOADS(FORCES)
MATRICES(MATHEMATICS)
Mechanics
STRESSES
STRUCTURAL PROPERTIES
TEMPERATURE
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:In preparation for the development of thermal capabilities into the fuselage analysis program, FUSARG, the thermal displacement column or H matrix for the idealized elements of this program were developed. The elements under consideration were the: (1) composite frame, (2) longitudinal effective flange, and (3) skin shear panel. The equations for the determination of stresses and deflection for a structure subjected to loads, temperature strains, and cutouts were developed. (Author)