Author: S. B. Batdorf
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 27
Book Description
A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Critical Combinations of Shear and Longitudinal Direct Stress for Long Plates with Transverse Curvature
Author: S. B. Batdorf
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 27
Book Description
A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 27
Book Description
A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Critical Combinations of Shear and Longitudinal Direct Stress for Long Plates with Tansverse Curvature
Author: S. B. Batdorf
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Critical Combinations of Longitudinal and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation
Author: S. B. Batdorf
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
A theoretical Investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal are presented that give the critical combinations of stress for several different degrees of elastic edge restraints Including simple support and complete fixity. It was found that an appreciable fraction of the critical longitudinal stress may be applied to the plate without any reduction in the transverse compressive stress required for buckling.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
A theoretical Investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal are presented that give the critical combinations of stress for several different degrees of elastic edge restraints Including simple support and complete fixity. It was found that an appreciable fraction of the critical longitudinal stress may be applied to the plate without any reduction in the transverse compressive stress required for buckling.
Critical Combinations of Shear and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation
Author: S. B. Batdorf
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Summary: An exact solution and a closely concurring approximate energy solution are given for the buckling of an infinitely long flat plate under combined shear and transverse direct stress with edges elastically restrained against rotation. It was found that an appreciable fraction of the critical stress in pure shear may be applied to the plate without any reduction in the transverse compressive stress necessary to produce buckling. An interaction formula in general use was shown to be decidedly conservative for the range in which it is supposed to apply.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Summary: An exact solution and a closely concurring approximate energy solution are given for the buckling of an infinitely long flat plate under combined shear and transverse direct stress with edges elastically restrained against rotation. It was found that an appreciable fraction of the critical stress in pure shear may be applied to the plate without any reduction in the transverse compressive stress necessary to produce buckling. An interaction formula in general use was shown to be decidedly conservative for the range in which it is supposed to apply.
Stability Analysis of Plates and Shells
Author:
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
Book Description
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
Book Description
Critical Combinations of Shear and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation
Author: Antonio Ferri
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 232
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Effect of Horizontal-tail Position on the Hinge Moments of an Unbalanced Rudder in Attitudes Simulating Spin Conditions
Author: Ralph W. Stone (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 560
Book Description
An investigation was made in the Langley 15-foot free-spinning tunnel to determine the effect of horizontal-tail position on rudder hinge-moments at attitudes simulating spinning conditions. Hinge-moment measurements were made on an unbalanced rudder on a rectangular vertical tail for six positions of the horizontail tail. The hinge-moment measurements were supplemented by tuft tests to determine the air flow about the vertical tail.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 560
Book Description
An investigation was made in the Langley 15-foot free-spinning tunnel to determine the effect of horizontal-tail position on rudder hinge-moments at attitudes simulating spinning conditions. Hinge-moment measurements were made on an unbalanced rudder on a rectangular vertical tail for six positions of the horizontail tail. The hinge-moment measurements were supplemented by tuft tests to determine the air flow about the vertical tail.
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 730
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 730
Book Description
Tests of Six Types of Bakelite-bonded Wire Strain Gages
Author: William R. Campbell
Publisher:
ISBN:
Category : Strain gages
Languages : en
Pages : 690
Book Description
Tests were made to determine the important performance characteristics for six types of bakelite-bonded wire strain gages commercially available and in current use by the aircraft industry. Results on the following characteristics are presented: (1) uniformity of calibration factors for individual gages of the same type, (2) variation of calibration factor with temperature, (3) creep, (4) effect of current on gage resistance, and (5) variation of gage resistance with temperature.
Publisher:
ISBN:
Category : Strain gages
Languages : en
Pages : 690
Book Description
Tests were made to determine the important performance characteristics for six types of bakelite-bonded wire strain gages commercially available and in current use by the aircraft industry. Results on the following characteristics are presented: (1) uniformity of calibration factors for individual gages of the same type, (2) variation of calibration factor with temperature, (3) creep, (4) effect of current on gage resistance, and (5) variation of gage resistance with temperature.