A 0.14-scale dynamically scaled model of the space shuttle orbiter wing was tested in the Langley Research Center 16-Foot Transonic Dynamics Wind Tunnel to determine flutter, buffet, and elevon buzz boundaries. Mach numbers between 0.3 and 1.1 were investigated. Rockwell shuttle model 54-0 was utilized for this investigation. A description of the test procedure, hardware, and results of this test is presented.
Results of Flutter Test OS6 Obtained Using the 0.14-Scale Wing/Elevon Model (54-0) in the NASA Larc 16-Foot Transonic Dynamics Wind Tunnel
1977
58 pages
Report
Keine Angabe
Englisch