naca-tn-962

  • Version
  • 61 Downloads
  • 2.57 MB File Size
  • 1 File Count
  • December 1, 2016 Create Date
  • December 1, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Analysis of Square Shear Web Above Buckling Load

naca-tn-962-analysis-of-square-shear-web-above-buckling-load-1

A solutiOn of Von Karman's fundamental equations for
plates with large deflections is presented for the case of
a shear web divided into square panels by reinforcing struts.
Numerical solutions are given for struts of infinite rigid—
ity and for struts the weight of which is one—fourth the
weight of the sheet. The results are compared with Wagner's
diagonal tension theory as extended by Kuhn and by Lnnghaar.
It is found that the diagonal tension theory as developed by
Kuhn agrees best with the present paper in the practical
range when r = 1/4, Kuhn's theory is in especially good
agreement for the force in the strut when r = 1/4.

The necessity for designing structures having the
smallest possible weight for a given lOad has forced air~
plane designers to build wing—beams and monoc0quc boxes
with sheer webs so thin that they may be buckled in a di-
agonnl direction under service loads. As the shear load is
increased well above the buckling lead, it is carried prin—
cipally by diagonal tension along the buckles, The beam
approaches a "diagonal-tension field" beam.

The lOad at which such shear webs will buckle has been
determined by several authors. (See, for example. pp. 357
to 568 of reference 1,) After buckling, the behavior of
the web is frequently determined frOm Wagner's diagonal—
tension—field theory (references 2 and 3) which neglects
the flexural rigidity of the sheet, Experimental results
(see p, 2 of reference 4, pp. 18 and 19 of reference 5, and
p. 5 of reference 6) indicate that Wagner's diagOnal—tension—
field theory may be too conservative for constructions in
which the diagonal tension field is only partially develOped.

An analysis of the behavior of a flat plate subjected
to shearing loads covering the range from the start of buck~
ling to the development of a full diagonal tension field was
therefore, thought desirable. Such an analysis, based 0n 2
Karman‘s large deflection equations' was made for the case or
a shear web divided into square panels by vertical struts.

FileAction
naca-tn-962 Analysis of Square Shear Web Above Buckling Load.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

naca-tn-962

  • Version
  • 61 Downloads
  • 2.57 MB File Size
  • 1 File Count
  • December 1, 2016 Create Date
  • December 1, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Analysis of Square Shear Web Above Buckling Load

naca-tn-962-analysis-of-square-shear-web-above-buckling-load-1

A solutiOn of Von Karman's fundamental equations for
plates with large deflections is presented for the case of
a shear web divided into square panels by reinforcing struts.
Numerical solutions are given for struts of infinite rigid—
ity and for struts the weight of which is one—fourth the
weight of the sheet. The results are compared with Wagner's
diagonal tension theory as extended by Kuhn and by Lnnghaar.
It is found that the diagonal tension theory as developed by
Kuhn agrees best with the present paper in the practical
range when r = 1/4, Kuhn's theory is in especially good
agreement for the force in the strut when r = 1/4.

The necessity for designing structures having the
smallest possible weight for a given lOad has forced air~
plane designers to build wing—beams and monoc0quc boxes
with sheer webs so thin that they may be buckled in a di-
agonnl direction under service loads. As the shear load is
increased well above the buckling lead, it is carried prin—
cipally by diagonal tension along the buckles, The beam
approaches a "diagonal-tension field" beam.

The lOad at which such shear webs will buckle has been
determined by several authors. (See, for example. pp. 357
to 568 of reference 1,) After buckling, the behavior of
the web is frequently determined frOm Wagner's diagonal—
tension—field theory (references 2 and 3) which neglects
the flexural rigidity of the sheet, Experimental results
(see p, 2 of reference 4, pp. 18 and 19 of reference 5, and
p. 5 of reference 6) indicate that Wagner's diagOnal—tension—
field theory may be too conservative for constructions in
which the diagonal tension field is only partially develOped.

An analysis of the behavior of a flat plate subjected
to shearing loads covering the range from the start of buck~
ling to the development of a full diagonal tension field was
therefore, thought desirable. Such an analysis, based 0n 2
Karman‘s large deflection equations' was made for the case or
a shear web divided into square panels by vertical struts.

FileAction
naca-tn-962 Analysis of Square Shear Web Above Buckling Load.pdfDownload 
17,005 Documents in our Technical Library
2863434 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...