Flow phenomena on plates and airfoils of short span (1936)
NASA Technical Reports Server (NTRS) · leaf 38
V.A.C.A. Technical Memorandum No. 798 Figs* 30,31,32,23 … ruction side of a flat rectangular plate, ' F/*2= 1/1.0; a = 27°. Figure 32.- Boundary-layer photograph of the suction side of a flat rectangular plate, F/b2= 1/0.5; a = 27°. ' Figure 33.* Smoke picture of the suction side of a flat rectengulax plate, F/l>2= 1/1.0; a = 45°. Separated flow. 3o
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