Wind Tunnel Tests of a 20-Gore Disk-Gap-Band Parachute
Abstract
This report documents wind tunnel tests of a series of 20 gore Disk- Gap-Band parachutes to determine the effects of gap length, band billow, and cloth air permeability on the parachute aerodynamic characteristics. Measurements for the steady-state drag-force, opening shock force, oscillation stability, and inflation stability were made of the various configurations and are presented in tabular and graphical format. Keywords: Disk gap-band- parachutes; Stability; Parachute technology; Opening shock; Design data; Geometric forms; Effects of geometry on aerodynamic properties.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 28, 1989
- Accession Number
- ADA221326
Entities
People
- William P. Ludtke
Organizations
- Naval Surface Warfare Center