Author: Bruno A. Boley
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 54
Book Description
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.
A Numerical Approach to the Instability Problem of Monocoque Cylinders
Author: Bruno A. Boley
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 54
Book Description
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.
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 54
Book Description
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.
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1512
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1512
Book Description
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 680
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 680
Book Description
List of Technical Notes, 1947-1953
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
Book Description
Airplane Structures: General design requirements
Author: Alfred Salem Niles
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
Stresses in and General Instability of Monocoque Cylinders with Cutouts
Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 64
Book Description
All but one cylinder failed in general instability. The one that did not show the general-instability pattern failed in tension.
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 64
Book Description
All but one cylinder failed in general instability. The one that did not show the general-instability pattern failed in tension.
Stresses in and General Instability of Monocoque Cylinders with Cutouts
Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Monocoque construction
Languages : en
Pages : 33
Book Description
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.
Publisher:
ISBN:
Category : Monocoque construction
Languages : en
Pages : 33
Book Description
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.