Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 68
Subjects: Plates (Engineering; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003804721&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003804721&ix=nu&I=0&V=D&pm=1</a>