Effect of variation in diameter and pitch of rivets on compressive strength of panels with z-section stiffeners.
Subtitle: I, panels with close stiffener spacing that fail by local buckling
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 18
Subjects: Rivets and riveting, Aircraft; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638639&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638639&ix=nu&I=0&V=D&pm=1</a>