Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2°
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 18
Subjects: Seaplanes--Hydrodynamics; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1</a>