Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 20
Subjects: Reynolds number; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638084&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638084&ix=nu&I=0&V=D&pm=1</a>