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naca-report-735

naca-report-735
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  • August 30, 2016 Create Date
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National Advisory Committee for Aeronautics, Report - Restraint Provided a Flat Rectangular Plate by a Sturdy Stiffener Along an Edge of the Plate

naca-report-735 Restraint Proveded a Flat Rectangular Plate vy a Sturdy Stiffener Along an Edge of the Plate-1

A sturdy stifle-nor is defined as a stifiener of such pro-
portions that it does not safer cross-sectional distortion
when moments are applied to some part of the cross
section. When such a stiflener is attached to one edge
of a plate, it will resist rotation of that edge of the plate
by means of its torsional properties. A formula is gire-n
for the restraint coeficient provided the plate by such a
stifener.

In the calculation of the critical compressive stress
for flat rectangular plates as presented in references 1
and 2, it is necessary first to evaluate the restraint
coefficient along an unloaded edge of the plate. The
formula that must. be used to evaluate this restraint
will depend upon the characteristics of the structural
member or members which provide the restraint. In
references 1 and 2 it was'assumcd that the restraint was
provided by a specially defined elastic restraining
medium. As a result of this assumption, it was
possible to derive a general design chart for the calcu—
lation of the critical compressive stress that is, within
wide limits, independent of the structure which
provides the restraint.

On the assumption of perfect elasticity, both 6 and
D are constant for the plate and it. is necessary to
evaluate only 3.3. The detailed effect of loading beyond
the elastic range is considered in another section of
this paper.

The basic property of the elastic restraining medium,
as used in the theory of references 1 and 2 in the defini—
tion of e, is that rotation at one point of the medium
does not affect rotation atanother point of the medium.
In. many practical problems the elastic restraint is
provided by a stiffener, a plate, or some other structure
for which rotation at one point does affect rotation at
another point. Consequently, the evaluation of So in
any given problem must take into account the effect of
this interaction Within the elastic restraining structure.

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naca-report-735

naca-report-735
  • Version
  • 326 Downloads
  • 373.65 KB File Size
  • 1 File Count
  • August 30, 2016 Create Date
  • August 30, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Restraint Provided a Flat Rectangular Plate by a Sturdy Stiffener Along an Edge of the Plate

naca-report-735 Restraint Proveded a Flat Rectangular Plate vy a Sturdy Stiffener Along an Edge of the Plate-1

A sturdy stifle-nor is defined as a stifiener of such pro-
portions that it does not safer cross-sectional distortion
when moments are applied to some part of the cross
section. When such a stiflener is attached to one edge
of a plate, it will resist rotation of that edge of the plate
by means of its torsional properties. A formula is gire-n
for the restraint coeficient provided the plate by such a
stifener.

In the calculation of the critical compressive stress
for flat rectangular plates as presented in references 1
and 2, it is necessary first to evaluate the restraint
coefficient along an unloaded edge of the plate. The
formula that must. be used to evaluate this restraint
will depend upon the characteristics of the structural
member or members which provide the restraint. In
references 1 and 2 it was'assumcd that the restraint was
provided by a specially defined elastic restraining
medium. As a result of this assumption, it was
possible to derive a general design chart for the calcu—
lation of the critical compressive stress that is, within
wide limits, independent of the structure which
provides the restraint.

On the assumption of perfect elasticity, both 6 and
D are constant for the plate and it. is necessary to
evaluate only 3.3. The detailed effect of loading beyond
the elastic range is considered in another section of
this paper.

The basic property of the elastic restraining medium,
as used in the theory of references 1 and 2 in the defini—
tion of e, is that rotation at one point of the medium
does not affect rotation atanother point of the medium.
In. many practical problems the elastic restraint is
provided by a stiffener, a plate, or some other structure
for which rotation at one point does affect rotation at
another point. Consequently, the evaluation of So in
any given problem must take into account the effect of
this interaction Within the elastic restraining structure.

FileAction
naca-report-735 Restraint Proveded a Flat Rectangular Plate by a Sturdy Stiffener Along an Edge of the Plate.pdfDownload 
17,005 Documents in our Technical Library
2642177 Total Downloads

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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 ...