Investigation of effect of sideslip on lateral stability characteristics.
Subtitle: II, rectangular midwing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 64
Subjects: Airplanes--Fuselage--Testing; Airplanes--Wings--Testing; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003620415&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003620415&ix=nu&I=0&V=D&pm=1</a>