Interference of Wing and Fuselage from Tests of 209 Combinations in the NACA Variable-Density Tunnel (1936)
NASA Technical Reports Server (NTRS) · leaf 7
. Consequently, the position was entirely outside the fuselage were tested in this way. corrected at angles of attack of 16° and —16° to give For these tests the wing was first mounted on the the correct gap and fore-and-aft position and the balance in the usual manner and the fuselage was… … (b) The fuselage on the balance. (a) The wing on the balance Figure 3—Set-ups in the tunnel for two typical disconnected combinations. NOT REPRODUCI BLE gap for each set-up was checked while the tunnel was The forces on the fuselage in the presence of the under pressure by varying the angle of wing…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
