Influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 80
Subjects: Airplanes--Testing; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003804754&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003804754&ix=nu&I=0&V=D&pm=1</a>