A gas (oxidizer) flows between two parallel walls of solid fuel. A combustion is initiated: the solid fuel is vaporized and a diffusive flame occurs. The hot combustion products are submitted both to thermal diffusion an...
The paper presents the development of numerical experiences using finite element commercial codes, based on experimental mechanical tests performed on ablative composite materials. The studied ablative materials were obt...
The aim of this paper is to produce and validate a simulated model of the external flow around the NACA 2412 using ANSYS Fluent; utilising experimental data for a low velocity case (20.73 m/s) from literature. This model...
In this paper, the wing on the Unmanned Aerial System UAS-S45 BĂ alam from Hydra Technologies is modeled and studied so that its aerodynamics and baseline performance can be better understood. More specifically, the perfo...
The main objective of this paper is to develop a set of tools and integrate techniques in a software package dedicated to stress analysis of aeronautical structures.
Analytical solutions for the temperature field in a 2D incompressible inviscid flow through a channel with walls of solid fuel
A gas (oxidizer) flows between two parallel walls of solid fuel. A combustion is initiated: the solid fuel is vaporized and a diffusive flame occurs. The hot combustion products are submitted both to thermal diffusion an...
Mechanical properties evaluation and model finite element analysis of cork and felt based nanofilled phenolic resin composites
The paper presents the development of numerical experiences using finite element commercial codes, based on experimental mechanical tests performed on ablative composite materials. The studied ablative materials were obt...
Investigation of the flow around an aircraft wing of section NACA 2412 utilising ANSYS fluent
The aim of this paper is to produce and validate a simulated model of the external flow around the NACA 2412 using ANSYS Fluent; utilising experimental data for a low velocity case (20.73 m/s) from literature. This model...
Simulation Study of the Aerodynamic Force Distributions on the UAS-S45 Baalam Wing with an Upswept Blended Winglet
In this paper, the wing on the Unmanned Aerial System UAS-S45 BĂ alam from Hydra Technologies is modeled and studied so that its aerodynamics and baseline performance can be better understood. More specifically, the perfo...
[b]INPROV - an environment for stress analysis of aeronautical structures[/b]
The main objective of this paper is to develop a set of tools and integrate techniques in a software package dedicated to stress analysis of aeronautical structures.