A series of simple wing/elevon flutter models of the shuttle orbiter were tested in a 26-inch transonic blowdown tunnel. Flutter points were obtained for two levels of scaled elevon actuator stiffness. A description of the wind tunnel models and the test procedures utilized in the experiment are given. (Author)
Flutter Tests (OS1) of the 0.02-Scale Shuttle Orbiter Wing/Elevon Semi-Span Model 230
1974
66 pages
Report
Keine Angabe
Englisch
Thermal analysis of Shuttle Orbiter wing/elevon seals
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