Experiments with a Wing Model from which the Boundary Is Removed by Suction (1929)
NASA Technical Reports Server (NTRS) · leaf 35
Figs. 32 & 33 Flow condi- tions accord- Fig*4 Test model for the preliminary ing to tests• (Section V) Fig.31, with & without suction. Suspen- sion of model in front of cone of small wind Al)b. 21 tunnel, shov;n in … ^Figs.21a & 211d Model in Section VIII-
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