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Accession Number:
AD0269493
Title:
WIND TUNNEL INVESTIGATION OF FLEXIBLE PARACHUTE MODELS AT SUPERSONIC SPEEDS
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN
Report Date:
1962-01-01
Abstract:
Tests were conducted in the 40-in. Supersonic Tunnel of the von Karman Gas Dynamics Facility to determine the aerodynamic characteristics of a series of flexible parachute models at Mach numbers from 1.5 to 3. Parachutes of various designs employing porous, non-porous, and ribbon materials were tested by deployment from a modified Pershing model. High-speed movies and drag measurements were obtained. Author
Pages:
0001
Contract Number:
AF40 600 800
File Size:
0.00MB
