Theory of propellers.
Subtitle: III, the slipstream contraction with numerical values for two-blade and four-blade propellers
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1944
Place of publication: Langley Field, VA
Language: eng
Number of pages: 112
Subjects: Propellers, Aerial; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638511&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638511&ix=nu&I=0&V=D&pm=1</a>