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Flexible Wing Cargo Gliders: Final program summary report
Ryan Aeronautical Company
出版U. S. Army Transportation Research Command, 1962
URLhttp://books.google.com.hk/books?id=-KWirdh9SyoC&hl=&source=gbs_api
EBookFULL_PUBLIC_DOMAIN
註釋The data contained herein presents the results of the study which relates to the performance of the towed air logistics gliders. Four basic configurations, with payload capacities of 250, 1,000, 4,000 and 8,000 lbs. each, were analyzed for towing and free-flight modes. Performance and flight characteristics of Army aircraft used for towing, both for tow and free of tow regimes, were also analyzed; and analysis of air drop configuration of 1,000 lb. payload capacity was made, with ejection and deployment time and motion study included.