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NASA-TR-R-279

NASA-TR-R-279
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  • 1.19 MB File Size
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  • April 21, 2016 Create Date
  • April 21, 2016 Last Updated
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Plastic Behaviour of Circular Plates Under Transverse Impulse Loadings of Gaussian Distribution
NASA-TR-R-279 Plastic Behaviour of Circular Plates Under Transverse Impulse Loadings of Gaussian Distribution
An analytical study of the plastic response of a circular plate of uniform thickness
subjected to a normal axisymmetric impulse of Gaussian distribution is presented. The
Gaussian impulse loading is assumed initially to impart a momentum to the plate. The
plate is thereafter prescribed as free from external loads. The kinetic energy of motion
is assumed to be dissipated in plastic deformation. The radial and circumferential
strain and strain—rate distributions of the plastically deforming plate are determined as
a function of time and space from derived deflection expressions. Only the bending
action of the plate is taken into account and the plate material is assumed to behave as a
perfectly plastic—rigid continuum.
The possibility of a fracture or separation of the plate material occurring during
deformation is discussed. Maximum values of strain and strain rate are shown to occur
in the circumferential components, and a mode of failure by radial fractures is indicated.
The impingement and fracture of the main wall of a space vehicle by meteoroids
are of major concern to the spacecraft designer. Protective devices, such as meteoroid
bumpers, have been proposed to shatter the impinging meteoroid and to lessen its pene-
trating potential. It has been shown both theoretically and experimentally (refs. 1 and 2)
that the resulting cloud of meteoroid and bumper debris passes on to the main wall of the
space vehicle as an impulsive loading having a general Gaussian distribution. A study
of the dynamic response of a plate under this impulsive type loading could well classify
the mode or manner of fracture at failure recently observed experimentally on double
sheet models of a bumper and main wall configuration. (See refs. 3 and 4.)
The information presented herein was included in a thesis submitted in partial ful-
fillment of the requirements for the degree of Doctor of Philosophy, Virginia Polytechnic
Institute, Blacksburg, Va., 1966.
A thorough analysis of the behavior of an impulsively loaded plate should include
not only the plastic but also the elastic response of the plate material. Because of the
complex time-dependent properties of the problem, however, most analyses consider
only the rigid—plastic response of the plate and neglect its elastic behavior entirely.

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NASA-TR-R-279

NASA-TR-R-279
  • Version
  • 56 Downloads
  • 1.19 MB File Size
  • 1 File Count
  • April 21, 2016 Create Date
  • April 21, 2016 Last Updated
Scroll for Details

Plastic Behaviour of Circular Plates Under Transverse Impulse Loadings of Gaussian Distribution
NASA-TR-R-279 Plastic Behaviour of Circular Plates Under Transverse Impulse Loadings of Gaussian Distribution
An analytical study of the plastic response of a circular plate of uniform thickness
subjected to a normal axisymmetric impulse of Gaussian distribution is presented. The
Gaussian impulse loading is assumed initially to impart a momentum to the plate. The
plate is thereafter prescribed as free from external loads. The kinetic energy of motion
is assumed to be dissipated in plastic deformation. The radial and circumferential
strain and strain—rate distributions of the plastically deforming plate are determined as
a function of time and space from derived deflection expressions. Only the bending
action of the plate is taken into account and the plate material is assumed to behave as a
perfectly plastic—rigid continuum.
The possibility of a fracture or separation of the plate material occurring during
deformation is discussed. Maximum values of strain and strain rate are shown to occur
in the circumferential components, and a mode of failure by radial fractures is indicated.
The impingement and fracture of the main wall of a space vehicle by meteoroids
are of major concern to the spacecraft designer. Protective devices, such as meteoroid
bumpers, have been proposed to shatter the impinging meteoroid and to lessen its pene-
trating potential. It has been shown both theoretically and experimentally (refs. 1 and 2)
that the resulting cloud of meteoroid and bumper debris passes on to the main wall of the
space vehicle as an impulsive loading having a general Gaussian distribution. A study
of the dynamic response of a plate under this impulsive type loading could well classify
the mode or manner of fracture at failure recently observed experimentally on double
sheet models of a bumper and main wall configuration. (See refs. 3 and 4.)
The information presented herein was included in a thesis submitted in partial ful-
fillment of the requirements for the degree of Doctor of Philosophy, Virginia Polytechnic
Institute, Blacksburg, Va., 1966.
A thorough analysis of the behavior of an impulsively loaded plate should include
not only the plastic but also the elastic response of the plate material. Because of the
complex time-dependent properties of the problem, however, most analyses consider
only the rigid—plastic response of the plate and neglect its elastic behavior entirely.

FileAction
NASA-TR-R-279 Plastic Behaviour of Circular Plates Under Transverse Impulse Loadings of Gaussian Distribution.pdfDownload 
17,005 Documents in our Technical Library
2727416 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 ...