Paulo Celso Greco Júnior

• A fast viscous correction method applied to be solution of the euler equations in two-dimensional transonic flow, AR.BR
• Frequency domain unsteady transonic aerodynamics for flutter and limit cycle oscillation prediction, AR.EXT

• Abstract

  This project is about the study of the behavior and the aerodynamic forces on a small-scale model of 14-Bis by experimental tests in a wind tunnel. The model of Santos Dumont’s historic aircraft was built between 2002 and 2003, after several researches about its characteristics. The theoretical study of the aircraft was done as well. Then, to validate the study, it needs to be done some t…

  Experimental analysis of aerodynamic forces, stability, and control, of 14-Bis by wind tunnel tests on a small-scale model, BP.IC

• Abstract

  This work involves using turbopump design methodologies, for pressurized liquid propellant injection, in static tests with small rocket engines. The turbopump will also be analyzed using Computational Fluid Dynamics software. This work is part of an effort to build a Space Engineering Laboratory in the Aeronautical Engineering Department of the School of Engineering of Sao Carlos, Univers…

  Simulation and Implementation of a methodology of design of a turbopump to be used in liquid propellant injection during rocket engine testing, BP.IC

• Abstract

  The capacity of gererating computational meshing, suitable for a domain discretization, is one of the most important factors to resolve problems using the CFD method. The goal of this project is to develop strategies to generate computational meshing - using several methods for a domain discretization - which are capable to describe the flow around the elements of rotors and stators of …

  Study of Strategies for Generation of Computational Meshing for CFD in Rotor-Stator Assemblies of Turbofan Engines., BP.IC

(Only some records are available in English at this moment)