In the aerospace industry one of the most important requirements in the aircraft design andoperation is the high level of fiability under various atmosphere and environmental conditions. Thedesign and validation of such a system is a great challenge. It must meet several requirements suchas: high resistence, low weight and a small occupied volume. The stresses that occur during theaircraft operation are extremely complex, being the result of the interaction of differentsystems.Consequently, in order to obtain an optimal design of the whole system, the design, testingand operating processes require a combination of laborious analysis and experimental data. As upto 90% of the structure failures are du to the fatigue, high performance methods ...
Aircraft structure is the most obvious example where structural efficiency results in light weight a...
Damage Tolerance method for structural integrity evaluation of helicopters fuselages requests a deta...
There the study objects are the statistic characteristics of appearance of fitigue macrocracks in th...
In the aerospace industry one of the most important requirements in the aircraft design and operatio...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
This thesis presents a new modeling framework and application methodology for the study of aircraft...
Aircraft airworthiness maintenance is carried out by a number of measures guaranteeing safe operatio...
This subject is connected with the structural health monitoring (SHM) of aircraft. Progressive metho...
Aircraft structural risk and reliability analysis has gained considerable interest in the area of ai...
The paper reviews the current state-of-the art of modern computational tools which can be adopted to...
The paper demonstrates a methodology that can be used at an early design stage of any conventional a...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
Onderhoud van vliegtuigen Descriptor(s) helicopter structural loads fatigue life A Modelling framewo...
In the last decades, the assessment of the service durability of aerospace components and assemblies...
Aircraft structure is the most obvious example where structural efficiency results in light weight a...
Aircraft structure is the most obvious example where structural efficiency results in light weight a...
Damage Tolerance method for structural integrity evaluation of helicopters fuselages requests a deta...
There the study objects are the statistic characteristics of appearance of fitigue macrocracks in th...
In the aerospace industry one of the most important requirements in the aircraft design and operatio...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
This thesis presents a new modeling framework and application methodology for the study of aircraft...
Aircraft airworthiness maintenance is carried out by a number of measures guaranteeing safe operatio...
This subject is connected with the structural health monitoring (SHM) of aircraft. Progressive metho...
Aircraft structural risk and reliability analysis has gained considerable interest in the area of ai...
The paper reviews the current state-of-the art of modern computational tools which can be adopted to...
The paper demonstrates a methodology that can be used at an early design stage of any conventional a...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
Onderhoud van vliegtuigen Descriptor(s) helicopter structural loads fatigue life A Modelling framewo...
In the last decades, the assessment of the service durability of aerospace components and assemblies...
Aircraft structure is the most obvious example where structural efficiency results in light weight a...
Aircraft structure is the most obvious example where structural efficiency results in light weight a...
Damage Tolerance method for structural integrity evaluation of helicopters fuselages requests a deta...
There the study objects are the statistic characteristics of appearance of fitigue macrocracks in th...