Scale Effect on Clark Y Airfoil Characteristics from NACA Full-Scale Wind-Tunnel Tests (1935)
NASA Technical Reports Server (NTRS) · leaf 6
gle of attack; the balance, any changes in the measured characteristics Reynolds Numbers of the tests are therefore slightly with the struts in place could be attributed to their different at the low and high angles of attack. A interference. A similar method was employed for the full discussion of… … Figure 3—Dummy supports added to the 8 by 48 airfoil set-up for interference tests.
NASA Technical Reports Server (NTRS)
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