The rapid development of hovercraft during the past decade has involved a concentrated effort on research and development to overcome the problems associated with a new form of transport. Some of the problems have not yet been solved and, in particular, the question of ride and stability characteristics is most important. An experimental and theoretical study has been made to achieve a method of prediction of stiffness and damping parameters through the change of cushion pressure during forcing of the cushion. [Continues.
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
In this study, a three degrees of freedom nonlinear air cushion vehicle (ACV) model is introduced to...
An experimental investigation was conducted to study rotor pitch damping in hover, axial flight (cli...
The handling qualities of hovercraft indicate the need for a better understanding of the influence ...
A first generation of commercial amphibious hovercraft has now been operating on a scheduled basis ...
A linearized theory of hovercraft response while moving over regular waves is modified to account fo...
This experimental study investigated the feasibility of applying the concept of a skirtless hovercra...
This experimental study investigated the feasibility of applying the concept of a skirtless hovercra...
Traveling in a hovercraft provides a unique means of travel. Advanced hovercraft designs allow the u...
grantor: University of TorontoThis thesis describes a theoretical investigation of the non...
The analytical tools (analysis and computer simulation) needed to explain and predict the dynamic op...
Research on the Steadiness and Controlablity of Hovercraft on Dinamic Cushion on Landing, Take- Off...
A fleet of civil tilt rotor transports offers a means of reducing airport congestion and point-to-po...
A program to develop analytical tools for evaluating the dynamic performance of Air Cushion Landing ...
The hovering performance and the lifting capability of tiltrotor aircraft are strongly affected by t...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
In this study, a three degrees of freedom nonlinear air cushion vehicle (ACV) model is introduced to...
An experimental investigation was conducted to study rotor pitch damping in hover, axial flight (cli...
The handling qualities of hovercraft indicate the need for a better understanding of the influence ...
A first generation of commercial amphibious hovercraft has now been operating on a scheduled basis ...
A linearized theory of hovercraft response while moving over regular waves is modified to account fo...
This experimental study investigated the feasibility of applying the concept of a skirtless hovercra...
This experimental study investigated the feasibility of applying the concept of a skirtless hovercra...
Traveling in a hovercraft provides a unique means of travel. Advanced hovercraft designs allow the u...
grantor: University of TorontoThis thesis describes a theoretical investigation of the non...
The analytical tools (analysis and computer simulation) needed to explain and predict the dynamic op...
Research on the Steadiness and Controlablity of Hovercraft on Dinamic Cushion on Landing, Take- Off...
A fleet of civil tilt rotor transports offers a means of reducing airport congestion and point-to-po...
A program to develop analytical tools for evaluating the dynamic performance of Air Cushion Landing ...
The hovering performance and the lifting capability of tiltrotor aircraft are strongly affected by t...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
In this study, a three degrees of freedom nonlinear air cushion vehicle (ACV) model is introduced to...
An experimental investigation was conducted to study rotor pitch damping in hover, axial flight (cli...