Title: Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1</a>
Subjects: Airplanes--Testing, Aerodynamics--Research.