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Fullscale wind tunnel investigation of the effects of a target type trust reverser on the low speed reverser on the low speed aerodynamic characreistics of asingle engine jet airplane [NASA TN D-72]

By: Contributor(s): Material type: TextTextLanguage: English Series: National Aeronautics and Space AdministrationPublication details: Washington, D. C. National Aeronautics and Space Administration 1959Description: 42pSubject(s):
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