Effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1943
Place of publication: Langley Field, VA
Language: eng
Number of pages: 56
Subjects: Propellers, Aerial; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003805344&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003805344&ix=nu&I=0&V=D&pm=1</a>