Hypotheses adopted for conventional ram-air gliding parachutes are not valid for paraglider aerodynamics and they require a new investigation. This paper presents an experimental database for a reference wing representative of a paraglider wing. Interest is focused on the external flow and on the influence of the spanwise arched shape on stationary longitudinal and lateral aerodynamic characteristics.To isolate this effect, leading edge intake and swell of real textile inflated cells are not represented. Thus,the reference wing is rigid and filled
An investigation has been made in the Langley 7- by 10-foot transonic tunnel to determine the subson...
In this study, the aerodynamic effects of the inflation of a paraglider wing (canopy) are investigat...
To come up with a new configuration for a hand launched Unmanned Aerial Vehicle (UAV ), the applicat...
A finite volume flow solver was used to solve the Reynolds averaged Navier-Stokes equations for the ...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
This project presents a basic wind tunnel investigation on aerodynamics of ram-air parafoils. Previo...
A low- speed wind-tunnel investigation was conducted to determine the effects of canopy construction...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
Wind tunnel test of canopy construction methods, design details, and canopy slots effects on aerodyn...
The objective of this work is the computational analysis of the in-flight deformation of a commercia...
An investigation has been made in the Langley 7- by 10-foot transonic tunnel to determine the subson...
Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leadin...
Paraglider sail (canopy) consists of a series of flexible boxes pressurized by special openings loca...
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of parag...
In the present study, we investigate the flow characteristics of a paraglider canopy with leading-ed...
An investigation has been made in the Langley 7- by 10-foot transonic tunnel to determine the subson...
In this study, the aerodynamic effects of the inflation of a paraglider wing (canopy) are investigat...
To come up with a new configuration for a hand launched Unmanned Aerial Vehicle (UAV ), the applicat...
A finite volume flow solver was used to solve the Reynolds averaged Navier-Stokes equations for the ...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
This project presents a basic wind tunnel investigation on aerodynamics of ram-air parafoils. Previo...
A low- speed wind-tunnel investigation was conducted to determine the effects of canopy construction...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
Wind tunnel test of canopy construction methods, design details, and canopy slots effects on aerodyn...
The objective of this work is the computational analysis of the in-flight deformation of a commercia...
An investigation has been made in the Langley 7- by 10-foot transonic tunnel to determine the subson...
Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leadin...
Paraglider sail (canopy) consists of a series of flexible boxes pressurized by special openings loca...
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of parag...
In the present study, we investigate the flow characteristics of a paraglider canopy with leading-ed...
An investigation has been made in the Langley 7- by 10-foot transonic tunnel to determine the subson...
In this study, the aerodynamic effects of the inflation of a paraglider wing (canopy) are investigat...
To come up with a new configuration for a hand launched Unmanned Aerial Vehicle (UAV ), the applicat...