In recent years, interest has been shown in jump-gliding devices. A few devices have been made that can successfully outperform a ballistic projectile using low Reynolds Number glides.This thesis presents the attempts to develop a high Reynolds Number jump-glider, using both prototyping means and modeling means. The descriptions of these processes include discussions on testing methods, computational trajectory models, and optimization fundamentals. This research has culminated in the framework of a tool that can be used to design optimal jump-gliders
In many aero gliding vehicles, achieving the maximum gliding range is a challenging task. A frequent...
Small UAV?s and flight vehicles in other atmospheres such as Mars are characterized by low Reynolds ...
Range optimal steady-state gliding is realized when the lift coefficient maximizes the lift-to-drag ...
In recent years, interest has been shown in jump-gliding devices. A few devices have been made that ...
Recent work suggests that jumping locomotion in combination with a gliding phase can be used as an e...
AbstractThis paper describes the concurrent optimization of the design of a discus and the skill wit...
Design of experiments and surrogate models method facilitating much of today's engineering design an...
Combining high precision numerical analysis methods with optimization algorithms to make a systemati...
abstract: This project is investigating the impact curvature, buckling, and anisotropy play when use...
The simulation presented in this thesis illustrates some of the basic mechanisms governing the winch...
i In this project a preliminary design of a self-launching system for the JS1 sailplane was attempte...
Thesis (M.Ing. (Mechanical Engineering)--North-West University, Potchefstroom Campus, 2010.In this p...
automatic adjustment user’s edit Figure 1: (Left) Our model airplane design tool analyzes the aerody...
Blended-Wing-Body Underwater Glider (BWBUG), which has excellent hydrodynamic performance, is a new ...
AbstractThis paper describes optimization of the size and launch conditions of a discus. The objecti...
In many aero gliding vehicles, achieving the maximum gliding range is a challenging task. A frequent...
Small UAV?s and flight vehicles in other atmospheres such as Mars are characterized by low Reynolds ...
Range optimal steady-state gliding is realized when the lift coefficient maximizes the lift-to-drag ...
In recent years, interest has been shown in jump-gliding devices. A few devices have been made that ...
Recent work suggests that jumping locomotion in combination with a gliding phase can be used as an e...
AbstractThis paper describes the concurrent optimization of the design of a discus and the skill wit...
Design of experiments and surrogate models method facilitating much of today's engineering design an...
Combining high precision numerical analysis methods with optimization algorithms to make a systemati...
abstract: This project is investigating the impact curvature, buckling, and anisotropy play when use...
The simulation presented in this thesis illustrates some of the basic mechanisms governing the winch...
i In this project a preliminary design of a self-launching system for the JS1 sailplane was attempte...
Thesis (M.Ing. (Mechanical Engineering)--North-West University, Potchefstroom Campus, 2010.In this p...
automatic adjustment user’s edit Figure 1: (Left) Our model airplane design tool analyzes the aerody...
Blended-Wing-Body Underwater Glider (BWBUG), which has excellent hydrodynamic performance, is a new ...
AbstractThis paper describes optimization of the size and launch conditions of a discus. The objecti...
In many aero gliding vehicles, achieving the maximum gliding range is a challenging task. A frequent...
Small UAV?s and flight vehicles in other atmospheres such as Mars are characterized by low Reynolds ...
Range optimal steady-state gliding is realized when the lift coefficient maximizes the lift-to-drag ...