Add to ORKGAnalysis of vortex generator's behavior and performance of flight tests in a given ultra-light aircraft model.- Theoretical study and state of the art of use of these devices. - Flow simulation across a given lifting surface with and without VGs. - Analysis of vortex generator’s performance in different configurations for given conditions.- Practical application: testing vortex generators into an experimental ultra-light aircraft and performing in-flight tests
An advanced engineering model has been developed to aid in the analysis and design of hydrogen/oxyge...
Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and...
ABSTRACT OF THE THESIS Numerical Simulation of flow Past NACA 0012 Airfoil Using a Co-Flow Jet at Di...
CFD and wind tunnel simulations are complementary due to their inherent limitations. Wind tunnel te...
The leading edge flow structure was investigated on a 70 deg flat plate delta wing which was pitched...
The main scope of this thesis is to have a strong tool for a preliminar design and sizing of an axia...
The mathematical model and associated computer program to simulate a twin-tailed high performance fi...
In this study, the aerodynamics of a one-degree-of-freedom wing motion, a constant speed pitch ramp,...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
The counter-rotating pair of wake vortices shed by flying aircraft can pose a threat to ensuing airc...
An experimental study of the wake of a turbulent boundary layer junction flow was performed using a ...
Hypersonic boundary layer measurements over a flared cone were conducted in a Mach 6 quiet wind tunn...
Despite advancements in our understanding of flight in modern times, birds remain unmatched when it ...
The aim of this project is to study the effect of different turbulence models on the detachment poin...
Swirling flows are complex fluid motions that appear in various natural phenomena and man-made devic...
An advanced engineering model has been developed to aid in the analysis and design of hydrogen/oxyge...
Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and...
ABSTRACT OF THE THESIS Numerical Simulation of flow Past NACA 0012 Airfoil Using a Co-Flow Jet at Di...
CFD and wind tunnel simulations are complementary due to their inherent limitations. Wind tunnel te...
The leading edge flow structure was investigated on a 70 deg flat plate delta wing which was pitched...
The main scope of this thesis is to have a strong tool for a preliminar design and sizing of an axia...
The mathematical model and associated computer program to simulate a twin-tailed high performance fi...
In this study, the aerodynamics of a one-degree-of-freedom wing motion, a constant speed pitch ramp,...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
The counter-rotating pair of wake vortices shed by flying aircraft can pose a threat to ensuing airc...
An experimental study of the wake of a turbulent boundary layer junction flow was performed using a ...
Hypersonic boundary layer measurements over a flared cone were conducted in a Mach 6 quiet wind tunn...
Despite advancements in our understanding of flight in modern times, birds remain unmatched when it ...
The aim of this project is to study the effect of different turbulence models on the detachment poin...
Swirling flows are complex fluid motions that appear in various natural phenomena and man-made devic...
An advanced engineering model has been developed to aid in the analysis and design of hydrogen/oxyge...
Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and...
ABSTRACT OF THE THESIS Numerical Simulation of flow Past NACA 0012 Airfoil Using a Co-Flow Jet at Di...