An investigation has been conducted to determine the opening charac-teristics of several hemispherical parachutes at airspeeds up to 200 miles per hour and to study the influence of the parachute design variables on these opening characteristics. The effects of design variables on the drag and stability characteristics of the parachutes were also evaluated. The tests were made in the Langley 20 foot free—spinning tunnel and in the Langley 300 MPH 7 — by 10—foot tunnel. Some of the parachutes blossomed fully when opened in the air stream. Beneficial effects on the parachute opening characteristics were obtained when longer shroud lines relative to parachute diameter were used, when the floating hem lines were tacked to prevent the hem—line l...
A test was conducted in the 16-ft Transonic Wind Tunnel of the Propulsion Wind Tunnel Facility to de...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
A team of researchers experimentally investigated the drag of several components of parachute suspen...
An investigation has been conducted to determine the opening characteristics of several hemispherica...
A drop-test investigation has been conducted to determine the stability and drag characteristics of ...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
A wind-tunnel investigation has been conducted to determine the parameters affecting the aerodynamic...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
Two Disk-Gap-Band model parachute designs were tested in the NASA Langley Transonic Dynamics Tunnel....
A test was conducted in the Propulsion Wind Tunnel (16T) of the Propulsion Wind Tunnel Facility to d...
Wind tunnel tests of recovery parachutes designed for controllable gliding fligh
A low- speed wind-tunnel investigation was conducted to determine the effects of canopy construction...
The performance characteristics of a preformed elliptical parachute at altitudes between 200,000 and...
A test was conducted in the 16-ft Transonic Wind Tunnel of the Propulsion Wind Tunnel Facility to de...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
A team of researchers experimentally investigated the drag of several components of parachute suspen...
An investigation has been conducted to determine the opening characteristics of several hemispherica...
A drop-test investigation has been conducted to determine the stability and drag characteristics of ...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
A wind-tunnel investigation has been conducted to determine the parameters affecting the aerodynamic...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect...
Two Disk-Gap-Band model parachute designs were tested in the NASA Langley Transonic Dynamics Tunnel....
A test was conducted in the Propulsion Wind Tunnel (16T) of the Propulsion Wind Tunnel Facility to d...
Wind tunnel tests of recovery parachutes designed for controllable gliding fligh
A low- speed wind-tunnel investigation was conducted to determine the effects of canopy construction...
The performance characteristics of a preformed elliptical parachute at altitudes between 200,000 and...
A test was conducted in the 16-ft Transonic Wind Tunnel of the Propulsion Wind Tunnel Facility to de...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
A team of researchers experimentally investigated the drag of several components of parachute suspen...