Title

Thermo-Structural Analysis Manual

Description

This second volume of the Thermo-Structural Analysis Manual considers additional problems in the field of thermal and mechanical stress analysis not fully treated in Volume I. Special emphasis is given to nonlinear analysis of beams and plates and to axisymmetric thermo-elastic analysis of thin shells. Following the format of Volume I, nondimensional graphs, formulas and tables are developed where feasible. For clarification of the analytical techniques and the use of the numerical data, illustrative examples are given.
The following problems are treated: (1) large deflection analysis of straight elastic beams with axial end restraint and axial end loads coupled with transverse loading and temperature, (2) approximate determination of the axal end loads and deformations in heated beam columns with initial eccentricities,(3) approximate solutions for the buckling of eccentric columns accommodating nonlinear stress strain laws, (4) axisymmetric large deflections of circular plates subjected to thermal and mechanical loads, and (5) axisymmetric thermo-elastic analysis of thin shells.

Date

1962

Index Abstract

Contrails and DTIC

Photo Quality

Not Needed

Report Number

WADD TR 60-517 Vol II

Creator

Forray, M. J.

Newman, M.

Switzky, H.

Corporate Author

Republic Aviation Corporation

Laboratory

Flight Dynamics Laboratory

Extent

214

Identifier

AD0290593

AD0290593

Access Rights

OTS

Distribution Classification

1

Contract

AF 33(616)-6066

DoD Project

1367

DoD Task

136710

DTIC Record Exists

Yes

Distribution Change Authority Correspondence

None

Distribution Conflict

No

Report Availability

Full text available by request

Date Issued

1962-10

Abstract

This second volume of the Thermo-Structural Analysis Manual considers additional problems in the field of thermal and mechanical stress analysis not fully treated in Volume I. Special emphasis is given to nonlinear analysis of beams and plates and to axisymmetric thermo-elastic analysis of thin shells. Following the format of Volume I, nondimensional graphs, formulas and tables are developed where feasible. For clarification of the analytical techniques and the use of the numerical data, illustrative examples are given.
The following problems are treated: (1) large deflection analysis of straight elastic beams with axial end restraint and axial end loads coupled with transverse loading and temperature, (2) approximate determination of the axal end loads and deformations in heated beam columns with initial eccentricities,(3) approximate solutions for the buckling of eccentric columns accommodating nonlinear stress strain laws, (4) axisymmetric large deflections of circular plates subjected to thermal and mechanical loads, and (5) axisymmetric thermo-elastic analysis of thin shells.

Provenance

Bombardier/Aero

Type

report

Subject

Airframes

Thermal Stresses

Stresses

Aircraft

Deformation

Structures

Shells (Structural Forms)

Mathematical Analysis

Buckling

Aerodynamic Loading

Metal Plates

Handbooks

Publisher

Wright-Patterson Air Force Base, OH : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command