Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 76
Subjects: Ailerons; Aerodynamics--Research.
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>