Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 46
Subjects: Aerofoils; Compressibility; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1</a>