Titre : |
Contributions to the Theory of Aircraft Structures |
Type de document : |
texte imprimé |
Auteurs : |
A. VAN DER NEUT |
Editeur : |
Delft University Press |
Année de publication : |
1972 |
Importance : |
440 p. |
Note générale : |
Preface
Contents
Biographical note
References |
Catégories : |
Structures Structures à parois minces
|
Index. décimale : |
620.1 Mécanique de l'ingénieur (mécanique appliquée) et matériaux |
Résumé : |
An appraisal of van der Neut's scientific work
Compression panels. An alternative language
Discussion of the mission analysis criterion for the definition of structural design loads
Structural safety of aircrafts
Some developments in structural airworthness requirements
Dynamic aspects of Fokker F-28 aircraft design
The application of the finite element displacement method to problems of elastoplastic deformation
On the diffusion of a load from a semi-infinite stringer bonded to a sheet
Stress concentration around holes in plates and shells
The bursting speed of a symmetrical conical diskwith radial holes
On the theory of multilayer shells
Stresses in a circular cylindrical shell with arbitrary holes
A general theory of isotensoid pressure vessels
Closed form solution to the semi-infinite cylindrical shell problem
Buckling of circular cylindrical shells under axial compression
The influence of production imperfections on design of optimum structures
Onthe perturbation method in the stability analysis of continuous systems
Optimum design of circular sandwich plates
On the transition from axisymmetric to multilobed creep buckling
Steady state equations of motion, equilibrium shape and stability derivatives of elastic airplanes evaluated with finite element methods
Buckling of integrally stiffenend cylindrical shells - A review of experiment and theory
Rationalization of anisotropic buckling problems
Brittle fracture under dynamic loading conditions
Calculation of potential flow about aerofoils using approximation by splines
On frequency shifting by elementary modifications of inertia and stiffness
Fatigue of lugs |