Alvaro Martins Abdalla.

Proposta que busca introduzir estudantes de graduação em problemáticas da cidade contemporânea, territórios do precário, junto a comunidades, articulando diferentes áreas de conhecimento

Information on shapes for low radar detection and aerodynamic requirements for supersonic flight are indispensable for the overall performance of military fighter aircraft during the conceptual and preliminary design.
The internship will consist of studies on generic aircraft models designed to demonstrate the importance of shape in the Radar Cross Section (RCS) of an aircraft. In addition, make it possible to identify the most vulnerable areas. However, the ideal project is to get an aircraft capable of surviving the mission. Therefore, it is necessary to have a balance between RCS and aerodynamics. 
The trainee will participate in the development and adaptation of computational tools that will work together with 3D CAD software (DASSAULT SYSTÈMES CATIA / SOLIDWORKS) to design, calculate and optimize stealth and aerodynamic parameters of the aircraft under analysis.

Busca se obter experimentalmente o RCS (radar cross section) ou assinatura de radar de uma aeronave em escala. Para isso será projetado e construído um mini radar e desenvolvido uma ferramenta computacional para cálculo e avaliação de RCS.

The project consists in designing and building a drone which can detect metal, from the air so that there is no damage in the aircraft, and analyze the data recollected from the flight to detonate landmines afterwards.
There are many countries in danger of landmine deaths, so it is our responsibility to solve this problem and to finish the threat they may cause. The purpose of this project is to prevent future damage in human race caused by the conclusions of past wars. For that, the development of a drone capable of detecting metals from the air will be a future solution to this problem.
Designing a drone with a small metal detector to map the dangerous area is the method I have used to solve this problem. Also, with the help of an computer tool Statistical Entropy study of the locations of these mines we have been able to work on this challenge.

Busca-se o desenvolvimento de dispositivos que evitem as aeronaves entrarem inadvertidamente na manobra parafuso ou que auxiliem a recuperação satisfatória da manobra parafuso quando provocada em aeronaves de aviação geral ou treinamento militar primário; dispositivos aerodinâmicos com alta confiabilidade e baixos valores em custo, peso estrutural e arrasto aerodinâmico.

This project aims to add a high fidelity tool, that calculates supersonic aerodynamic coefficients, on SANCA program that was developed earlier by Prof. Alvaro Abdalla (EESC-USP) in your Post-Doctoral work at the Linköping University / Sweden. The tool should establish current and new methodologies that predict aerodynamic coefficients at supersonic conditions. For new methodologies wind tunnel and CFD data will be referenced to validate the method. The tool will be developed by coordinated activates among Linköping University (LiU ), School of Engineering of São Carlos (EESC-USP), Technological Institute of Aeronautics (ITA), SAAB and EMBRAER.

SwedenThe project should be done in partnership should be classified as a continuity to the project already developed earlier when Post-Doctoral work at the Linköping University / Sweden and the implement of the work currently under development for Supersonic Aerodynamics module in SANCA program.
At the Linköping University partners should be open to discussion to implement Supersonic Aerodynamics module in SANCA program. This module should apply existing methodologies to supersonic parasite drag calculation and also the new methodology being developed.
Then, along with researchers from Linköping University, will be integrated and interacted to Hopsan program / LiU and other modules or codes could be developed.

- Projeto de perfil aerodinâmico da asa
- Projeto da geometria da asa
- Projeto da winglet da asa.