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Flugmechanik
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Tests of Vortex-Ring Parachute at Supersonic Speed in the Langley Unitary Plan Wind Tunnel
Aerodynamic Characteristics of Parachutes at Mach Numbers from 1.6 to 3
Aerodynamic Heating and Deceleration During Entry into Planetary Atmospheres
Performance of a 16.6 Meter Diameter Modified Ringsail Parachute in a Simulated Martian Environment
Performance of a 16.6 Meter Diameter Cross Parachute in a Simulated Martian Environment
Performance of a 19.7 Meter Diameter Disk-Gap-Band Parachute in a Simulated Martian Environment
Overview of the LaNCETS Flight Experiment and CFD Analysis. Supplemental Movies
Aeroelastic Control of a Segmented Trailing Edge Using Fiber Optic Strain Sensing Technology