For purpose of providing standard airfoil characteristics for use in airplane design, Material Division of Army Air Corps requested that six airfoils having commonly used sections be tested in variable-density wind tunnel; results of tests.
Tests of three tapered airfoils based on N.A.C.A. 2200 N.A.C.A.-M6, and Clark Y sections
Nat Advisory Committee Aeronautics -- Tech Note
1934
8 pages
5 Supp plates
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Tests of N.A.C.A. Airfoils in variable-density wind tunnel
Engineering Index Backfile | 1936
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