A simple method for predicting the uniaxial compression strength of laminated composites containing impact damages is presented. The method is based on a simplified model of the damage zone and a fracture criterion originally developed for notched laminates. This approach allows to derive a closed-form equation expressing the post-impact strength as a function of the damage size and damage intensity. The properties of the damaged laminate are characterized by two parameters which have to be determined from experimental data. Some examples are given showing that the predicted strength is in good agreement with test results. (orig.)Available from TIB Hannover: RR 2088(19-93 PUB)ME / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische ...
In this paper, the damaged area in fibre-reinforced quasi-isotropic laminates that have been subject...
An efficient numerical approach for the prediction of the Compression After Impact (CAI) strength of...
International audienceThis paper deals with impact damage, permanent indentation and compression aft...
ABSTRACT: A new method to determine the compression after impact (CAI) strength of composite laminat...
Today the use of composite materials in the aircraft industry is very widespread also for the primar...
Low-velocity impact damage can drastically reduce the residual mechanical properties of the composit...
ABSTRACT: Tests are conducted using stitched laminates in order to calculate the unnotched failure s...
Impact damage has been known to seriously limit the performance of composite aircraft structures. In...
Nonvisible impact damage reduces static and residual strength of cfrp-composite structures. Fatigue ...
Low-velocity impact damage can drastically reduce the residual strength of a composite structure eve...
International audienceA numerical approach is presented to estimate the compressive behaviors of 150...
Some aspects of a problem mechanical, mainly, impact damage of a composite material and their influ...
A full-scale model for predicting low-velocity impact (LVI) damage and compression after impact (CAI...
The paper presents two methods for predicting the in-plane compression strength of impact damaged sa...
International audienceThe development and certification of aeronautical composite structures is stil...
In this paper, the damaged area in fibre-reinforced quasi-isotropic laminates that have been subject...
An efficient numerical approach for the prediction of the Compression After Impact (CAI) strength of...
International audienceThis paper deals with impact damage, permanent indentation and compression aft...
ABSTRACT: A new method to determine the compression after impact (CAI) strength of composite laminat...
Today the use of composite materials in the aircraft industry is very widespread also for the primar...
Low-velocity impact damage can drastically reduce the residual mechanical properties of the composit...
ABSTRACT: Tests are conducted using stitched laminates in order to calculate the unnotched failure s...
Impact damage has been known to seriously limit the performance of composite aircraft structures. In...
Nonvisible impact damage reduces static and residual strength of cfrp-composite structures. Fatigue ...
Low-velocity impact damage can drastically reduce the residual strength of a composite structure eve...
International audienceA numerical approach is presented to estimate the compressive behaviors of 150...
Some aspects of a problem mechanical, mainly, impact damage of a composite material and their influ...
A full-scale model for predicting low-velocity impact (LVI) damage and compression after impact (CAI...
The paper presents two methods for predicting the in-plane compression strength of impact damaged sa...
International audienceThe development and certification of aeronautical composite structures is stil...
In this paper, the damaged area in fibre-reinforced quasi-isotropic laminates that have been subject...
An efficient numerical approach for the prediction of the Compression After Impact (CAI) strength of...
International audienceThis paper deals with impact damage, permanent indentation and compression aft...