Effects of wing elasticity on the aerodynamic characteristics of an airplane configuration having 45 degrees sweptback wings as obtained from free-flight rocket-model tests at transonic speeds Page: 1 of 50
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EFFECTS OF WING ELASTICITY ON THE AERODYNAMIC
CHARACTERISTICS OF AN AIRPLANE CONFIGURATION HAVING
S45 SWEPTBACK WINGS AS OBTAINED FROM FREE -FLIGHT
' $ ROCKET-MODEL TESTS AT TRANSONIC SPEEDS
By A. James Vitale
Langley Aeronautical Laboratory
I . Langley Field, Va.
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S January 28, 1953
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Vitale, A. James. Effects of wing elasticity on the aerodynamic characteristics of an airplane configuration having 45 degrees sweptback wings as obtained from free-flight rocket-model tests at transonic speeds, report, January 28, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59504/m1/1/: accessed March 25, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.