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Author: Bruno A. Boley
Publisher:
Published: 1951
Total Pages: 54
ISBN-13:
DOWNLOAD EBOOK →A procedure similar to the first method was developed for a calculation of the buckling load of a cylinder with a cutout. A limitded experimental check was obtained.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1951
Total Pages: 1462
ISBN-13:
DOWNLOAD EBOOK →Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1950
Total Pages: 1464
ISBN-13:
DOWNLOAD EBOOK →Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1945
Total Pages: 1512
ISBN-13:
DOWNLOAD EBOOK →Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1954
Total Pages: 162
ISBN-13:
DOWNLOAD EBOOK →Author: Nicholas John Hoff
Publisher:
Published: 1949
Total Pages: 64
ISBN-13:
DOWNLOAD EBOOK →All but one cylinder failed in general instability. The one that did not show the general-instability pattern failed in tension.
Author: Nicholas John Hoff
Publisher:
Published: 1948
Total Pages: 33
ISBN-13:
DOWNLOAD EBOOK →Stresses were calculated by a numerical method in three reinforced monocoque cylinders subjected to pure bending. The cylinders were of circular cross section and were reinforced with 8 rings and either 8 or 16 stringers. There was a cutout on one side of each cylinder located symmetrically to the neutral plane and extending over 45, 90, and 135 degrees. Satisfactory agreement was found between stresses calculated and those measured in Part 4 of the present series of investigations.
