Add to ORKGCompilation of methods of solution for thermal stress problems of types frequently encountered by aircraft designers. The following problem areas are addressed: problems within limits of linear elastic theory, complex linear problems and problems involving non-linearity."August 1962"Includes bibliographical references.Compilation of methods of solution for thermal stress problems of types frequently encountered by aircraft designers. The following problem areas are addressed: problems within limits of linear elastic theory, complex linear problems and problems involving non-linearity.Research supported by the United States Air Force Aeronautical Systems Division, and performed by the Republic Aviation Corporation, Framingdale, New York, und...
There the study objects are the non-uniform three-dimensional constructions of unspecified structure...
INTRODUCTION Integrated analysis methods can substantially reduce the time and effort required to pr...
The field of thermomechanical activities of DLR in numerical and experimental analysis of aerospace ...
This second volume of the Thermo-Structural Analysis Manual considers additional problems in the fie...
A collocation formulation is used as the basis for a unified approach to the various quasi static ae...
This book contains the elements of the theory and the problems of Elasticity and Thermal Stresses wi...
The stress problem of Prithvi missile wing is investigated .\ud The analysis is carried out by the f...
The Encyclopedia of Thermal Stresses is an important interdisciplinary reference work. In addition ...
Formulations for a general theory of thermoelasticity to generate accurate thermal stresses for stru...
Thermal Stress Analysis of Beams, Plates and Shells presents classic and advanced thermal stress top...
Includes bibliographical references (pages [70])The original STRESS computer program is modified by ...
A solution is derived for the thermal stresses in a finite cylindrical solid composed of a material ...
Additional information was added to a growing data base from which estimates of finite element model...
THE kinetic heating associated with supersonic flight produces temperature gradients within the air...
FEATS computer code uses finite element analysis to calculate steady state temperature and thermal s...
There the study objects are the non-uniform three-dimensional constructions of unspecified structure...
INTRODUCTION Integrated analysis methods can substantially reduce the time and effort required to pr...
The field of thermomechanical activities of DLR in numerical and experimental analysis of aerospace ...
This second volume of the Thermo-Structural Analysis Manual considers additional problems in the fie...
A collocation formulation is used as the basis for a unified approach to the various quasi static ae...
This book contains the elements of the theory and the problems of Elasticity and Thermal Stresses wi...
The stress problem of Prithvi missile wing is investigated .\ud The analysis is carried out by the f...
The Encyclopedia of Thermal Stresses is an important interdisciplinary reference work. In addition ...
Formulations for a general theory of thermoelasticity to generate accurate thermal stresses for stru...
Thermal Stress Analysis of Beams, Plates and Shells presents classic and advanced thermal stress top...
Includes bibliographical references (pages [70])The original STRESS computer program is modified by ...
A solution is derived for the thermal stresses in a finite cylindrical solid composed of a material ...
Additional information was added to a growing data base from which estimates of finite element model...
THE kinetic heating associated with supersonic flight produces temperature gradients within the air...
FEATS computer code uses finite element analysis to calculate steady state temperature and thermal s...
There the study objects are the non-uniform three-dimensional constructions of unspecified structure...
INTRODUCTION Integrated analysis methods can substantially reduce the time and effort required to pr...
The field of thermomechanical activities of DLR in numerical and experimental analysis of aerospace ...