No abstract available
The Characteristics of the N.A.C.A 97, Clark Y, and N.A.C.A. M6 Airfoils with Particular Reference to the Angle of Attack
01.12.1927
Sonstige
Keine Angabe
Englisch
Tests of three tapered airfoils based on N.A.C.A. 2200 N.A.C.A.-M6, and Clark Y sections
Engineering Index Backfile | 1934
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