Effect on helicopter performance of modifications in profile-drag characteristics of rotor-blade airfoil sections
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1944
Place of publication: Langley Field, VA
Language: eng
Number of pages: 42
Subjects: Laminar flow; Rotors (Helicopters; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003617559&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003617559&ix=nu&I=0&V=D&pm=1</a>