A drop-test investigation has been conducted to determine the stability and drag characteristics of radially vented (duplex) parachutes. Parachutes of two different designs were tested: a large parachute with high geometric porosity and a small parachute with low geometric porosity designed for the same descent velocity with the same load. The results of the tests show that the large high-porosity duplex parachute was very stable in descent, oscillations averaging about [plus-or-minus]3.4⁰; and the average drag coefficient based on the total canopy area and based on the fabric area alone were approximately 0.38 and 0.55, respectively. The small, low-porosity duplex parachute was also very stable in descent, oscillations averaging about [plu...
A team of researchers experimentally investigated the drag of several components of parachute suspen...
Wind tunnel tests of recovery parachutes designed for controllable gliding fligh
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
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 ...
An investigation has been conducted to determine the opening charac-teristics of several hemispheric...
The Low Density Supersonic Decelerator Project is developing a next-generation supersonic parachute ...
An investigation was conducted at Mach 1.80 in the Langley 4-foot supersonic pressure tunnel to dete...
Supersonic wind-tunnel tests were conducted with disk-gap-band parachute models having a nominal dia...
Ten flight tests of modified-ringsail, disk-gap-band, and cross parachute configurations with deploy...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
Free-body tests of flat circular parachutes and determination of aerodynamic drag coefficients durin...
Two Disk-Gap-Band model parachute designs were tested in the NASA Langley Transonic Dynamics Tunnel....
A wind-tunnel investigation has been conducted to determine the parameters affecting the aerodynamic...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
A team of researchers experimentally investigated the drag of several components of parachute suspen...
Wind tunnel tests of recovery parachutes designed for controllable gliding fligh
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
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 ...
An investigation has been conducted to determine the opening charac-teristics of several hemispheric...
The Low Density Supersonic Decelerator Project is developing a next-generation supersonic parachute ...
An investigation was conducted at Mach 1.80 in the Langley 4-foot supersonic pressure tunnel to dete...
Supersonic wind-tunnel tests were conducted with disk-gap-band parachute models having a nominal dia...
Ten flight tests of modified-ringsail, disk-gap-band, and cross parachute configurations with deploy...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
Free-body tests of flat circular parachutes and determination of aerodynamic drag coefficients durin...
Two Disk-Gap-Band model parachute designs were tested in the NASA Langley Transonic Dynamics Tunnel....
A wind-tunnel investigation has been conducted to determine the parameters affecting the aerodynamic...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
A team of researchers experimentally investigated the drag of several components of parachute suspen...
Wind tunnel tests of recovery parachutes designed for controllable gliding fligh
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...