Static longitudinal stability and dynamic characteristics at high angles of attack and at low Reynolds numbers of a model of the X-3 supersonic research airplane Page: 1 of 77
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STATIC LONGITUDINAL STABILITY AND DYNAMIC CHARACTERISTICS
AT HIGH ANGLES OF ATTACK AND AT LOW REYNOLDS NUMBERS OFA MODEL OF THE X-3 SUPERSONIC RESEARCH AIRPLANE
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By Sanger M. Burk, Jr., and Burton E. IIultz
Langley Aeronautical Laboratory
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States, appropriate cvllan officers ad employees of the Federa Onernmet who have a legitmate Interest
therein, and to Unhited States citizens of known loyalty ad discretion who of neces ty mst be Informed thereof.NATIONAL ADVISORY COMMITTE
FOR AERONAUTICS A
WASHINGTON A.February 6, 1951
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Burk, Sanger M., Jr. & Hultz, Burton E. Static longitudinal stability and dynamic characteristics at high angles of attack and at low Reynolds numbers of a model of the X-3 supersonic research airplane, report, February 6, 1951; (https://digital.library.unt.edu/ark:/67531/metadc58742/m1/1/: accessed April 23, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.