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NASA RESEARCH ON FLEXIBLE WINGS

1968; Wiley; Volume: 154; Issue: 2 Linguagem: Inglês

10.1111/j.1749-6632.1968.tb15238.x

1749-6632

F. M. Rogallo,

Space Exploration and Technology

Annals of the New York Academy of SciencesVolume 154, Issue 2 p. 953-961 NASA RESEARCH ON FLEXIBLE WINGS Francis M. Rogallo, Francis M. Rogallo NASA Langley Research Center Langley Station, Hampton, Va.Search for more papers by this author Francis M. Rogallo, Francis M. Rogallo NASA Langley Research Center Langley Station, Hampton, Va.Search for more papers by this author First published: November 1968 https://doi.org/10.1111/j.1749-6632.1968.tb15238.xCitations: 1AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL REFERENCES 1 MAKULOWICH, 2/LIEUTENANT MICHAEL. 1966. Project “Flexwing. Sky-Diver Magazine. 8(5): 18– 19. 2 HAMILTON, J. SCOTT. 1966. Flight of the parawing. Parachutist Magazine. 7(9): 5– 10. 3 ROGALLO, FRANCIS M. & GERTRUDE S. ROGALLO. 1951. U.S. Patent No. 2, 546, 078. 4 ROGALLO, FRANCIS M. 1951. First flexible kite. Ford Times Magazine 43: 25– 30. 5 ROGALLO, FRANCIS M. 1963. Parawings for Astronautics. Presented at the Specialist Meeting on Space Rendezvous, Rescue, and Recovery. Cosponsored by Am. Astronaut. Soc. & Air Force Flight Test Center. Edwards Air Force Base, Calif. 16 (Part 2): 3– 11. 6 ROGALLO, FRANCIS M., JOHN G. LOWRY, DELWIN R. CROOM & ROBERT T. TAYLOR. 1960. Preliminary investigation of a paraglider. NASA T N D-443. 7 SLEEMAN, WILLIAM D., Jr. 1963. Low-speed investigation of cable tension and aerodynamic characteristics of a parawing and spacecraft combination. NASA TN D-1937. 8 CROOM, DELWIN R., RODGER L. NAESETH & WILLIAM C. SLEEMAN, Jr. 1964. Effects of canopy shape on low-speed aerodynamic characteristics of a 55° swept parawing with large-diameter leading edges. NASA TN D-2551. 9 LIBBEY, CHARLES E. 1963. Free-flight investigation of the deployment of a parawing recovery device for a radio-controlled 1/5-scale dynamic model spacecraft. NASA TN D-2044. 10 LAYTON, GARRISON P. & MILTON O. THOMPSON. 1963s. Preliminary flight evaluation of two unpowered manned paragliders. NASA TN D-1826. 11 JOHNSON, JOSEPH L., Jr. 1962. Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. NASA TN D-1255. 12 JOHNSON, JOSEPH L., JR. & JAMES L. HASSELL, Jr. 1963. Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle. NASA TN D-1946. 13 SHANKS, ROBERT E. 1964. Experimental investigation of the dynamic stability of a towed parawing glider air cargo delivery system. NASA TN D-2292. 14 BURK, SANGER M., JR. 1963. Free-flight investigation of the deployment, dynamic stability, and control characteristics of a 1/12-scale dynamic radio-controlled model of a large booster and parawing. NASA TN D-1932. 15 POLHAMUS, EDWARD C. & RODGER L. NAESETH. 1963. Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having nominal aspect ratios of 3 and 6. NASA TN D-972. 16 BUGG, FRANK M. 1965. Effects of aspect ratio and canopy shape on low-speed aerodynamic characteristics of 50.0° swept parawings. NASA TN D-2922. Citing Literature Volume154, Issue2International Congress on Subsonic AeronauticsNovember 1968Pages 953-961 ReferencesRelatedInformation