Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1

An edition of Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1 (1986)

Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1

By M. Khalid

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Publish Date

1986

Publisher

National Aeronautical Establishment

Language

Pages

Description:

subjects: Reynolds number, Drag, Supersonic airfoils