Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1944
Place of publication: Langley Field, VA
Language: eng
Number of pages: 24
Subjects: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research.; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1</a>