Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

An edition of Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil (1945)

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

By Langley Aeronautical Laboratory

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Publish Date

1945

Publisher

Langley Memorial Aeronautical Laboratory

Language

eng

Pages

Description:

<a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1</a>

subjects: Ailerons, Aerodynamics--Research.