Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9 Page: 1 of 43
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CONTROL EFFECTIVENESS LOAD AND HINGE-MOMENT
CHARACTERISTICS OF A TIP CONTROL SURFACE
ON A DELTA WING AT A MACH NUMBER OF 1.9
By D. William Conner and Ellery B. May, Jr.
Langley Aeronautical Laboratory
Langley Air Force Base, Va.
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NATIONAL ADVISORY COMATTEE
FOR AERONAUTICS ,
October 7, 1949
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Conner, D. William & May, Ellery B., Jr. Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9, report, October 7, 1949; (https://digital.library.unt.edu/ark:/67531/metadc58388/m1/1/: accessed May 23, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.