Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Monocoque construction
Languages : en
Pages : 696
Book Description
Formulas for the calculation of influence coefficients of curved beams of constant radius of curvature are presented corresponding to displacements in the plane of curvature. Moreover, numerical values are given in tabular and graphicform for a limited number of values of the parameters involved.
Numerical Procedures for the Calculation of Stresses in Monocoques
Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Monocoque construction
Languages : en
Pages : 696
Book Description
Formulas for the calculation of influence coefficients of curved beams of constant radius of curvature are presented corresponding to displacements in the plane of curvature. Moreover, numerical values are given in tabular and graphicform for a limited number of values of the parameters involved.
Publisher:
ISBN:
Category : Monocoque construction
Languages : en
Pages : 696
Book Description
Formulas for the calculation of influence coefficients of curved beams of constant radius of curvature are presented corresponding to displacements in the plane of curvature. Moreover, numerical values are given in tabular and graphicform for a limited number of values of the parameters involved.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 856
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 856
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Applied Mechanics Reviews
Simply Supported Long Rectangular Plate Under Combined Axial Load and Normal Pressure
Author: Samuel Levy
Publisher:
ISBN:
Category : Axial loads
Languages : en
Pages : 738
Book Description
The results indicate it to be conservative design in the elastic range to neglect the effect of lateral pressure on the sheet buckling load and on the load carried by the sheet after buckling.
Publisher:
ISBN:
Category : Axial loads
Languages : en
Pages : 738
Book Description
The results indicate it to be conservative design in the elastic range to neglect the effect of lateral pressure on the sheet buckling load and on the load carried by the sheet after buckling.
Applicability of Similarity Principles to Structural Models
Author: James Norman Goodier
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 766
Book Description
A systematic account is given in Part 1 of the use of dimensional analysis in constructing similarity conditions for models and structures. The analysis covers large deflections, buckling, plastic behavior, and materials and nonlinear stress-strain characteristics, as well as the simpler structural problems. Part 2 deals with the testing of square plaes in shear, with and without holes.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 766
Book Description
A systematic account is given in Part 1 of the use of dimensional analysis in constructing similarity conditions for models and structures. The analysis covers large deflections, buckling, plastic behavior, and materials and nonlinear stress-strain characteristics, as well as the simpler structural problems. Part 2 deals with the testing of square plaes in shear, with and without holes.
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 34
Book Description
An Investigation of Aircraft Heaters
Author: Llewellyn Michael Kraus Boelter
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 666
Book Description
An analysis is presented of the factors determining the power efficiency of radiation thermopiles of that type in which the receivers consist either of parts of the conductors themselves or of coatings or other electrically insulating materials in intimate contact with these conductors. On the basis of this analysis, which is applicable to thermopiles of a wide variety of constructions and materials, criterions for maximum power efficiency can be calculated. Such criterions are obtained for a silver-constantan plated-type thermopile. The design and construction of thermopiles in accordance with these criterions are described, and test data are reported, showing agreement between actual and predicted performance.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 666
Book Description
An analysis is presented of the factors determining the power efficiency of radiation thermopiles of that type in which the receivers consist either of parts of the conductors themselves or of coatings or other electrically insulating materials in intimate contact with these conductors. On the basis of this analysis, which is applicable to thermopiles of a wide variety of constructions and materials, criterions for maximum power efficiency can be calculated. Such criterions are obtained for a silver-constantan plated-type thermopile. The design and construction of thermopiles in accordance with these criterions are described, and test data are reported, showing agreement between actual and predicted performance.
NACA Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 734
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 734
Book Description