A low- speed wind-tunnel investigation was conducted to determine the effects of canopy construction methods, design details, and canopy slots on the static longitudinal aerodynamic characteristics of all-flexible parawings. Construction details such as type of nonporous canopy fabric, glued or sewed seams, tape reinforcement, or cloth-weave orientation had little effect on maximum lift-drag ratios and resultant-force coefficients. The maximum lift-drag ratios varied from 2.2 to 2.5 for the various single-keel unslotted parawings, and from 2.2 to 2.4 for the slotted canopy parawings. Incremental reductions in the lengths of all the suspension lines caused corresponding reductions in the resultantforce coefficients and maximum lift-drag rat...
The FASTWing CL ram-air parafoil was designed for fully autonomous aerial deliveries of heavy payloa...
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
As the scale factor applied in the design of wind tunnel models is reduced, many details of the conf...
Wind tunnel test of canopy construction methods, design details, and canopy slots effects on aerodyn...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
A low-speed wind-tunnel investigation was conducted to study effects of wing-canopy shape on the aer...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
Longitudinal and lateral stability and control characteristics of tension-structure parawing
The deployment characteristics of a 1/8-size dynamically and elastically scaled model of an inflatab...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
Low speed wind tunnel tests of all-flexible twin-keel tension structure parawing
Wind tunnel and flight tests to determine aerodynamic characteristics and rigging control of flexibl...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
An investigation has been conducted to determine the opening charac-teristics of several hemispheric...
This project presents a basic wind tunnel investigation on aerodynamics of ram-air parafoils. Previo...
The FASTWing CL ram-air parafoil was designed for fully autonomous aerial deliveries of heavy payloa...
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
As the scale factor applied in the design of wind tunnel models is reduced, many details of the conf...
Wind tunnel test of canopy construction methods, design details, and canopy slots effects on aerodyn...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
A low-speed wind-tunnel investigation was conducted to study effects of wing-canopy shape on the aer...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
Longitudinal and lateral stability and control characteristics of tension-structure parawing
The deployment characteristics of a 1/8-size dynamically and elastically scaled model of an inflatab...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
Low speed wind tunnel tests of all-flexible twin-keel tension structure parawing
Wind tunnel and flight tests to determine aerodynamic characteristics and rigging control of flexibl...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
An investigation has been conducted to determine the opening charac-teristics of several hemispheric...
This project presents a basic wind tunnel investigation on aerodynamics of ram-air parafoils. Previo...
The FASTWing CL ram-air parafoil was designed for fully autonomous aerial deliveries of heavy payloa...
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
As the scale factor applied in the design of wind tunnel models is reduced, many details of the conf...