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Flexible Wing Light Utility Glider
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Book Synopsis FLEXIBLE WING LIGHT UTILITY GLIDER. by : N. SAKAMOTO
Download or read book FLEXIBLE WING LIGHT UTILITY GLIDER. written by N. SAKAMOTO and published by . This book was released on 1966 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented in the report are the results of a flight test program of a towed light utility glider system. The system was designed to carry odd-geometry cargo, and demonstrated towed flight operations up to the maximum design weight of 1500 pounds, at a velocity range extending from 30 to 70 knots indicated airspeed. Testing also included takeoff and landings on tow with helicopters, and evaluation of the flight homing system. Free flights of the light utility glider were also made carrying a payload of 800 pounds. Presented also are the system description, and an aerodynamic and structural analysis. (Author).
Book Synopsis FLEXIBLE-WING PRECISION DROP GLIDER. by : RYAN AERONAUTICAL CO SAN DIEGO CALIF.
Download or read book FLEXIBLE-WING PRECISION DROP GLIDER. written by RYAN AERONAUTICAL CO SAN DIEGO CALIF. and published by . This book was released on 1963 with total page 147 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flexible-wing paraglider concept was investigated as a means of controlled cargo delivery from either fixed-wing aircraft or rotary-wing aircraft to a predetermined landing site. Fullscale inflatable wings and control platforms were designed, fabricated, and flight tested. Specific areas of investigation included packing methods, launch techniques, deployment, transition from the parachute mode into the wing, controllability, glider performance, ground station manual control techniques, and automatic-home control evaluation. Considerable testing was directed toward determining the optimum packing method and deployment technique in an effort to achieve system reliability and toward effective system control in an effort to achieve minimum circular-error-probability. The feasibility of using the flexible-wing glider as a controllable means for cargo delivery to a predetermined landing site was successfully demonstrated. A flight envelope, encompassing allowable limits of airspeed, altitude and payload, was established for the final configuration of the series. (Author).
Book Synopsis Flexible Wing Cargo Gliders: Final program summary report by : Ryan Aeronautical Company
Download or read book Flexible Wing Cargo Gliders: Final program summary report written by Ryan Aeronautical Company and published by . This book was released on 1962 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Flexible Wing Cargo Gliders by : Ryan Aeronautical Company
Download or read book Flexible Wing Cargo Gliders written by Ryan Aeronautical Company and published by . This book was released on 1962 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flexible Wing Cargo Gliders: Design criteria and aerodynamics by : Ryan Aeronautical Company
Download or read book Flexible Wing Cargo Gliders: Design criteria and aerodynamics written by Ryan Aeronautical Company and published by . This book was released on 1962 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flexible Wing Precision Drop Glider by : Ryan Aeronautical Company
Download or read book Flexible Wing Precision Drop Glider written by Ryan Aeronautical Company and published by . This book was released on 1963 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flexible-wing paraglider concept was investigated as a means of controlled cargo delivery from either fixed-wing aircraft or rotary-wing aircraft to a predetermined landing site. Fullscale inflatable wings and control platforms were designed, fabricated, and flight tested. Specific areas of investigation included packing methods, launch techniques, deployment, transition from the parachute mode into the wing, controllability, glider performance, ground station manual control techniques, and automatic-home control evaluation. Considerable testing was directed toward determining the optimum packing method and deployment technique in an effort to achieve system reliability and toward effective system control in an effort to achieve minimum circular-error-probability. The feasibility of using the flexible-wing glider as a controllable means for cargo delivery to a predetermined landing site was successfully demonstrated. A flight envelope, encompassing allowable limits of airspeed, altitude and payload, was established for the final configuration of the series. (Author).
Book Synopsis Flexible Wing Towed Universal Glider by :
Download or read book Flexible Wing Towed Universal Glider written by and published by . This book was released on 1967 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Army Aviation Digest written by and published by . This book was released on 1963 with total page 1376 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1989 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis RC light-wind glider by : Dr. Heinrich Eder
Download or read book RC light-wind glider written by Dr. Heinrich Eder and published by Verlag für Technik und Handwerk. This book was released on with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flying from upwind to upwind without propulsion and fighting for every metre of height – that is the fascination of pure gliding. If you want to enjoy this without the electric drive that is so common today, you should pay attention to a few things when building your models. The author, Dr. Heinrich Eder, is a specialist in the aerodynamic peculiarities of light-wind gliders, and in this book, he makes his research results and experience available to everyone. Where do you place the turbulator, how do you calculate the setting angle difference, how do you optimally design winglets or find the best wing geometry? This technical book answers such questions and imparts the knowledge needed to design and optimise one's own constructions, with many photos, diagrams, and drawings. In addition, there is tried and tested advice for stable lightweight construction and successful flight, as well as many examples of proven light-wind gliders. From the content: • Re-number influence on sink rate • The induced drag • The wing aspect ratio of a light wind glider • How to calculate the EWD? • C.G. position and lift distribution • Winglets, Tiplets and Co. • Optimisation of lift distribution • Pitch and sweep • Profiles for light wind gliders • Selection of balsa and CFRP • Paper, polyester fleece and silk • Detecting and avoiding distortions • The effect of the turbulator • Running, rubber and winch launching • Descent aids and thermal tactics • Examples for light wind sailors
Book Synopsis Flexible Wing Individual Drop Glider by : Ryan Aeronautical Company
Download or read book Flexible Wing Individual Drop Glider written by Ryan Aeronautical Company and published by . This book was released on 1963 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: The feasibility of the paraglider concept as a means of descent for individual airborne troops is presented. Full-scale 22-foot inflatable wings and instrumented dummies were designed, fabricated, and flight tested to demonstrate this feasibility. Specific areas of investigation included packing method, deployment, transition from the parachute mode into the wing, controllability, glider performance, and the human tolerance aspect in relation to opening shock, landing loads, and velocities. Considerable testing was directed toward determining the best packing method and deployment technique in an effort to achieve system reliability. The feasibility of using the paraglider as a means of controlled delivery of airborne paratroopers was sucessfully demonstrated. (Author).
Download or read book Army Research and Development written by and published by . This book was released on 1963 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis FLEXIBLE WING INDIVIDUAL DROP GLIDER. by : B. E. Kurz
Download or read book FLEXIBLE WING INDIVIDUAL DROP GLIDER. written by B. E. Kurz and published by . This book was released on 1963 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: The feasibility of the paraglider concept as a means of descent for individual airborne troops is presented. Full-scale 22-foot inflatable wings and instrumented dummies were designed, fabricated, and flight tested to demonstrate this feasibility. Specific areas of investigation included packing method, deployment, transition from the parachute mode into the wing, controllability, glider performance, and the human tolerance aspect in relation to opening shock, landing loads, and velocities. Considerable testing was directed toward determining the best packing method and deployment technique in an effort to achieve system reliability. The feasibility of using the paraglider as a means of controlled delivery of airborne paratroopers was sucessfully demonstrated. (Author).
Download or read book Proceedings written by and published by . This book was released on 1972 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Operational Demonstration and Evaluation of the Flexible Wing Precision Drop Glider in Thailand, March-july 1963 by : William R. Quinn
Download or read book Operational Demonstration and Evaluation of the Flexible Wing Precision Drop Glider in Thailand, March-july 1963 written by William R. Quinn and published by . This book was released on 1963 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt: An operational demonstration and evaluation is made of the Ryan Flexible Wing Precision Drop in Thailand during March-July 1963. Thirty five drops were made. The glider is a radio-controlled aerial delivery system deployed from an aircraft with the capability of delivering a 300 lb payload to a designated landing zone at night or in all-weather conditions. The system consists of three main components: a reinforced cardboard cargo container, an aluminum control box, and a folded inflatable wing housed in the recessed center of the control box. In a packed, ready for flight condition, the system measures 24x32x48 inches and weighs approximately 386 lb. The high lift capability of the glider wing permits a 3.1 to 1 glide ratio, allowing a horizontal offset of 3.1 ft for every foot of altitude. This permits the pilot to release the cargo some distance away from the drop zone, avoiding enemy fire, unfavorable terrain, and disclosure of the position of friendly forces at the drop zone to the enemy. Horizontal offset can be increased or decreased depending on location of the drop aircraft in relation to the wind. The wing has a fixed rate of descent for a given cargo weight which can be increased by steep turns. It is about 11 ft/sec for a 300-lb payload. (Author).
Book Synopsis U.S. Government Research & Development Reports by :
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1014 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Army RD & A. written by and published by . This book was released on 1964 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt:
