Accession Number : AD0465108
Title : AERODYNAMIC CHARACTERISTICS OF THE PARACHUTE STABILIZED A-21 CARGO CONTAINER.
Descriptive Note : Final rept., Apr 63-Jul 64,
Corporate Author : MINNESOTA UNIV MINNEAPOLIS DEPT OF AERONAUTICS AND ENGINEERING MECHANICS
Personal Author(s) : Ibrahim, Shukry K.
Report Date : APR 1965
Pagination or Media Count : 48
Abstract : A study was conducted to determine the basic aerodynamic coefficients of the aerial delivery system of the A-21 cargo container and the optimum parachute-riser configurations for its stabilization during the high velocity stage of the delivery. A method was developed whereby system characteristics could be synthesized from the characteristics of the system components. The methods and information set forth in this report make it possible to determine, to a close approximation, the moment characteristics of many system configurations and to indicate, in terms of specified static stabilization criteria, the most critical configuration of the A-21 container system. Conversely, the method enables the parachute size to be calculated if the system stability characteristics as well as the parachute type and riser length are specified. Also, systems using the Ribless Guide Surface, Ring-Slot and Ribbon parachutes are compared on the basis of equal free stream drag area, parachute diameters to satisfy specified stabilization criteria and over-all system drag. (Author)
Descriptors : , (*CONTAINERS, AERODYNAMIC CHARACTERISTICS), (*CARGO PARACHUTES, STABILITY), (*AIR DROP OPERATIONS, CONTAINERS), AIRBORNE, OPTIMIZATION, MOMENTS, DRAG, STABILIZATION, PARACHUTE DESCENTS, WIND TUNNEL MODELS, MODEL TESTS, VELOCITY, ANGLE OF ATTACK, CORDAGE, WAKE, OSCILLATION, SCATTERING, EXPERIMENTAL DATA, TABLES(DATA), GRAPHICS, RIBBON PARACHUTES, AERODYNAMIC CONFIGURATIONS.
Distribution Statement : APPROVED FOR PUBLIC RELEASE