The subject of the study in the article is the problem of the exact forming of individual panels in the wingbox assembling process without technological spanwise joints of the wing. The goal of the study is to create a model for an oblique curvature forming of the stiffened panels, which provides high tolerance of the panel shape and a given position of the bending axis. Objectives: a development of procedures that improve the tolerance of panel forming, reduce the amount of fitting work, reduce labor intensity, and increase productivity. The methods include: local deformation forming method by means of applying bending moments at the sweep angle and an additional correction angle, which takes into account the elastic effects of the stiffen...
This paper presents the results of experimental and numerical analysis in terms of the finite elemen...
Structural weight has always been important in aircraft manufacturing industry. Considering that a l...
The mathematical model relations for buckling investigation of structurally-anisotropic panels made ...
This paper presents the results of experimental research on the fabrication of thin-walled panels wi...
There the purposes are to study the slow deforming process of ribbed panels, to develop the software...
Electromagnetic forming (EMF), as a high-speed forming technology by applying the electromagnetic fo...
International audienceThe aim of this article is to present and to analyze the capabilities of a pro...
Creep-age forming (CAF) is an interesting process for the airframe industry, as it is able to form o...
The questions of obtaining the profiles of high stiffness by using the bend with tangential compress...
In the article, the authors present a method of constrained bending of aircraft sheet parts with cur...
Creep-age forming (CAF) is an interesting process for the airframe industry, as it is able to form o...
Stiffened thin panels are very common and important structural elements in aerospace structures beca...
The article discusses questions of shaping honeycomb panels for turbojet engine noise insulation cas...
Abstract- Stiffened panel is a component in aircraft that is used to fasten the stiffener and the sk...
Press-braking bending is widely applied in the manufacture of aircraft integral panels because of th...
This paper presents the results of experimental and numerical analysis in terms of the finite elemen...
Structural weight has always been important in aircraft manufacturing industry. Considering that a l...
The mathematical model relations for buckling investigation of structurally-anisotropic panels made ...
This paper presents the results of experimental research on the fabrication of thin-walled panels wi...
There the purposes are to study the slow deforming process of ribbed panels, to develop the software...
Electromagnetic forming (EMF), as a high-speed forming technology by applying the electromagnetic fo...
International audienceThe aim of this article is to present and to analyze the capabilities of a pro...
Creep-age forming (CAF) is an interesting process for the airframe industry, as it is able to form o...
The questions of obtaining the profiles of high stiffness by using the bend with tangential compress...
In the article, the authors present a method of constrained bending of aircraft sheet parts with cur...
Creep-age forming (CAF) is an interesting process for the airframe industry, as it is able to form o...
Stiffened thin panels are very common and important structural elements in aerospace structures beca...
The article discusses questions of shaping honeycomb panels for turbojet engine noise insulation cas...
Abstract- Stiffened panel is a component in aircraft that is used to fasten the stiffener and the sk...
Press-braking bending is widely applied in the manufacture of aircraft integral panels because of th...
This paper presents the results of experimental and numerical analysis in terms of the finite elemen...
Structural weight has always been important in aircraft manufacturing industry. Considering that a l...
The mathematical model relations for buckling investigation of structurally-anisotropic panels made ...