[HTML][HTML] Performance analysis of composite ply orientation in aeronautical application of unmanned aerial vehicle (UAV) NACA4415 wing
The advancement in today's material science has driven composite materials to globally use
in aircraft design with its superiority in high structural stiffness and significant weight …
in aircraft design with its superiority in high structural stiffness and significant weight …
Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application
A finite element (FE) model is developed to study the structural performance on a composite
wing of a UAV with a tubercle design at the leading edge of the wing. The experimental …
wing of a UAV with a tubercle design at the leading edge of the wing. The experimental …
[HTML][HTML] Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle
A finite element model is developed to determine deformation and stresses on a composite
wing of unmanned aerial vehicle (UAV) with a tubercle design at the leading edge of the …
wing of unmanned aerial vehicle (UAV) with a tubercle design at the leading edge of the …
Structural optimization of a light aircraft composite wing
This paper presents the results of structural optimization of a two-spar composite wing for a
light aircraft. Different lay-up structures of power components such as spars, ribs and skin …
light aircraft. Different lay-up structures of power components such as spars, ribs and skin …
Performance analysis of composite laminates wing skin with the aid of fluid structure interaction of aerodynamic loading-structural analysis
Advances in today's technology have led to the use of composite materials with their
advantages of significant high strength with lightweight structure in aircraft design …
advantages of significant high strength with lightweight structure in aircraft design …
[PDF][PDF] Structural analysis of a transport aircraft wing
Y Abbas, T Elsonni, AA Abdulmajid, A Khalafallh… - Incas …, 2021 - bulletin.incas.ro
In this study the procedures of structural analysis of a typical transport aircraft wing has been
followed. The wing model has been drawn using CATIA® V5; this model consists of several …
followed. The wing model has been drawn using CATIA® V5; this model consists of several …
Design and analysis of a tail sitter (VTOL) UAV composite wing
In recent years the design and development of various classes of unmanned aerial vehicles
(UAV's) has grown significantly. It is a well-known fact that the utilization of composite …
(UAV's) has grown significantly. It is a well-known fact that the utilization of composite …
Effect of Cut-out shape on the stresses in aircraft wing ribs under aerodynamic load
Ribs in aircraft wings maintain the airfoil shape of the wing under aerodynamic loads and
also support the resulting bending and shear loads that act on the wing. Aircrafts are …
also support the resulting bending and shear loads that act on the wing. Aircrafts are …
Static Structural Analysis of Fighter Aircraft's Wing Spars
U Tariq, F Mazhar - 2021 International Bhurban Conference on …, 2021 - ieeexplore.ieee.org
This study aims at describing a methodology for the Static Structural Analysis of Fighter
Aircraft's wing spars for identification of critical stresses. Aircraft's wing is subjected to …
Aircraft's wing spars for identification of critical stresses. Aircraft's wing is subjected to …
Free vibration analysis of composite aircraft wing
As the aerospace industry continually seeks to enhance the performance and efficiency of
aircraft structures, the implementation of advanced materials such as composites has …
aircraft structures, the implementation of advanced materials such as composites has …