Two models were tested, one with symmetrical airfoil sections and other with same basic thickness forms but with reflex cambered mean line.
Effect of reflex chamber on aerodynamic characteristics of highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000
Nat Advisory Committee Aeronautics -- Tech Note
1947
10 pages
13 Supp Plates
Report
Englisch
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Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing
Online Contents | 2011
|Swept-tapered-wing aerodynamics
NTRS | 1976
|