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Summary of spin technology as related to light general-aviation airplanes

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:01:45Z
date available2017-09-04T16:01:45Z
date copyright01/01/1971
date issued1971
identifier otherRLYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/64983
description abstractA summary was made of all NASA (and NACA) research and experience related to the spin and recovery characteristics of light personal-owner-type general-aviation airplanes. Very little of the research deals with light general-aviation airplanes as such, but many of the airplanes and models tested before and during World War II were similar to present-day light general-aviation airplanes with regard to the factors that are important in spinning. The material is based mainly on the results of spin-tunnel tests of free-spinning dynamically scaled models of about 100 different airplane designs and, whenever possible, includes correlation with full-scale spin tests. The research results are discussed in terms of airplane design considerations and the proper use of controls for recovery.
languageEnglish
titleNASA-TN-D-6575num
titleSummary of spin technology as related to light general-aviation airplanesen
typestandard
page35
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1971
contenttypefulltext


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