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Flat Circular Plates
see also
Circular Plates
Flat Plates
Under Normal Pressure
stresses and large deflections for various edge conditions, 65003
Flat Disc Springs
see
Disc Springs
Flat Elliptical Plates
see
Elliptical Plates
Flat Plates
Semi-elliptical Plates
Flat Orthotropic Rectangular Plates
see
Circular Holes in Orthotropic Plates
Flat Specially-orthotropic Rectangular Plates
Flat Strips of Orthotropic Materials
Flat Unbalanced Laminated Rectangular Plates
Laminated Construction Using Composites
Noise
Flat Panels in General
see also
Flat Panels with Fibre-reinforced Unflanged Integral Stiffeners
Flat Panels with Flanged Integral Stiffeners
Flat Panels with Lipped or Unlipped Z-section Stiffeners
Flat Panels with Top-hat Section Stiffeners
Flat Panels with Transverse Stiffeners
Flat Panels with T-section Integral Stiffeners
Flat Panels with Unflanged Integral Stiffeners
Flat Panels with Unlipped Z-section Stiffeners
Flat Parallelogram Panels
Flat Parallelogram Plates
Flat Plates
Flat Sandwich Panels (Cores of Negligible Flexural Stiffness)
Flat Sandwich Panels (Corrugated Cores)
Flat Sandwich Panels (Isotropic Cores)
Flat Sandwich Panels (Truss Cores)
Sandwich Panels and Plates
Damping Ratio Values
typical values for composite, integrally-machined or skin/stringer, 91012
variation with frequency, 73011
Dynamic Response
mode shapes of vibrating, 72003
natural frequencies for flexible stringers, 73013
natural frequencies for stringers stiff in bending, 72003
Dynamic Response to Excitation
see also
Integrally-machined Panels
Panels
Response of Lightweight Structures
Skin-rib Joints in Aluminium Alloys
Skin-rib Joints in Composite Structures
Skin-rib Joints in Titanium Alloys
considerations in design against acoustic loading, 86025
effect of edge reinforcement on stresses due to acoustic loading, 67029
estimation of stresses due to acoustic loading for flexible stringers, 73014
estimation of stresses due to acoustic loading for stringers stiff in bending, 67028, 72005
Load Diffusion
coefficient of diffusion, STRUCT 02.05.00
introduction, STRUCT 02.05.00
Load Diffusion From Edge Members Under Constant Antisymmetrical Edge Strains
edge shear stresses and moment carried, STRUCT 02.05.00
Load Diffusion From Edge Members Under Constant Strain
average stresses in stringers and edge shear stresses, STRUCT 02.05.00
Load Diffusion From Edge Members Under Linearly Varying Strain
average stresses in stringers, STRUCT 02.05.00
Load Diffusion From Uniform Edge Members Under Concentrated End Loads
average stresses in stringers and edge shear stresses, STRUCT 02.05.00
Load Diffusion From Uniform Edge Members Under Linearly Increasing Edge Loads
average stresses in stringers, STRUCT 02.05.00
Load Diffusion From Uniform Edge Members Under Uniformly Distributed Edge Loads
average stresses in stringers, STRUCT 02.05.00
Modal Density
rectangular, isotropic, 11008
specially orthotropic, 11008
Post Buckling Analysis Under Shear
comprehensive worked example, 77014
compressive stress in stiffeners, 77014
description of flexural, local and torsional-flexural buckling, 72012
diagonal tension factor, 77018
flange bending moment due to diagonal tension field, 77014
flange end load due to diagonal tension field, 77014
prediction of stiffener failure by buckling, inter-rivet buckling or forced crippling, 77014
resultant loading on flange-to-plate and stiffener-to-flange joints, 77014
secant and tangent moduli of panel, 77014
stress for onset of plate yielding away from edges, 77014
stress for plate failure at flange-to-plate joint or away from edges, 77014
Under Compression (Uniaxial)
inter-rivet buckling, 72012, STRUCT 02.01.08, STRUCT 02.01.09
introduction and example of analysis, 72012
local and overall buckling load including effect of skin-rib jointing method, 98016
local and overall buckling load with stiffeners of any section shape, 98016
local buckling stresses, 72012, 73007, STRUCT 02.01.28, STRUCT 02.01.35, STRUCT 02.01.36
possible stiffness bands after buckling and effect of initial irregularities, 72012
strength of stringer in flexure, STRUCT 02.01.16, STRUCT 02.01.17
torsional and torsional-flexural buckling load with stiffeners of any section, 99016
torsional buckling load including effect of skin-rib jointing method, 99016
torsional-flexural buckling load including effect of skin-rib jointing method, 99016
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of skin-rib jointing method, 01001
local and overall buckling load with stiffeners of any section, 01001
torsional and torsional-flexural buckling load with stiffeners of any section, 01001
torsional buckling load including effect of skin-rib jointing method, 01001
torsional-flexural buckling load including effect of skin-rib jointing method, 01001
Under Shear
stresses for buckling and failure of castellations, STRUCT 02.03.24
Use of Layered Damping Materials to Increase Panel Damping
see also
Damping
constrained multi-layer treatment, 91012, 91013
constrained single layer treatment, 91012, 91013
free layer treatment, 91012, 91013
Flat Panels with Fibre-reinforced Unflanged Integral Stiffeners
see also
Flat Panels in General
Under Compression (Biaxial)
local buckling stress, 73015
Flat Panels with Flanged Integral Stiffeners
see also
Flat Panels in General
Integrally-machined Panels
Under Compression (Uniaxial), 72012, 83044
local buckling stress, 71014, 72012
local, overall, torsional and torsional-flexural buckling load, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local buckling stress, 71014, 72012, 83044
local, overall, torsional and torsional-flexural buckling load, 01001
Flat Panels with Lipped or Unlipped Z-section Stiffeners
Under Compression (Uniaxial)
local and overall buckling load including effect of skin-rib jointing method, 98016
local and overall buckling, machined or rolled-sheet stiffeners, 98016
torsional buckling load including effect of skin-rib jointing method, 98016
torsional buckling load, machined or rolled sheet stiffeners, 98016
torsional-flexural buckling load including effect of skin-rib jointing method, 98016
torsional-flexural buckling load, machined or rolled sheet stiffeners, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of skin-rib jointing method, 01001
local and overall buckling load, machined or rolled sheet stiffeners, 01001
torsional buckling load including effect of skin-rib jointing method, 01001
torsional buckling load, machined or rolled sheet stiffeners, 01001
torsional-flexural buckling load including effect of skin-rib jointing method, 01001
torsional-flexural buckling load, machined or rolled sheet stiffeners, 01001
Flat Panels with Top-hat Section Stiffeners
see also
Flat Panels in General
Under Compression (Uniaxial)
local and overall buckling load including effect of skin-rib jointing method, 98016
local and overall buckling load, machined or rolled-sheet stiffeners, 98016
local buckling stress, 72012, STRUCT 02.01.36
torsional buckling load including effect of skin-rib jointing method, 98016
torsional buckling load, machined or rolled sheet stiffeners, 98016
torsional-flexural buckling load including effect of skin-rib jointing method, 98016
torsional-flexural buckling load, machined or rolled sheet stiffeners, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of skin-rib jointing method, 01001
local and overall buckling load, machined or rolled sheet stiffeners, 01001
torsional buckling load including effect of skin-rib jointing method, 01001
torsional buckling load, machined or rolled sheet stiffeners, 01001
torsional-flexural buckling load including effect of skin-rib jointing method, 01001
torsional-flexural buckling load, machined or rolled sheet stiffeners, 01001
Flat Panels with Transverse Stiffeners
see also
Flat Panels in General
Under Shear
buckling stress, STRUCT 02.03.02
Flat Panels with T-section Integral Stiffeners
see also
Flat Panels in General
Integrally-machined Panels
Under Compression (Uniaxial)
local buckling stress, 71014, 72012
local, overall, torsional and torsional-flexutal buckling load, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local buckling stress, 72012, 77014, 83044
local, overall, torsional and torsional-flexural buckling load, 01001
Flat Panels with Unflanged Integral Stiffeners
see also
Flat Panels in General
Integrally-machined Panels
Noise
Under Compression (Uniaxial)
effect of initial irregularities on minimum weight design, 70007
local buckling stress, 70003, 72012, STRUCT 02.01.34
local, overall, torsional and torsional-flexural buckling load, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local buckling stress, 70003, 72012, 83044
local, overall, torsional and tosional-flexural buckling load, 01001
minimum weight design (with dimensional restriction), 70007
Flat Panels with Unlipped Z-section Stiffeners
see also
Flat Panels in General
Under Compression (Uniaxial)
example of analysis, 72012
local and ovearall buckling load including effect of skin-rib jointing method, 98016
local and overall buckling load, machined or rolled sheet stiffeners, 98016
local buckling stress, 71014, 72012, STRUCT 02.01.35
torsional buckling load including effect of skin-rib jointing method, 98016
torsional buckling load, machined or rolled sheet stiffeners, 98016
torsional-flexural buckling load including effect of skin-rib jointing method, 98016
torsional-flexural buckling load, machined or rolled sheet stiffeners, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of skin-rib jointing method, 01001
local and overall buckling load, machined or rolled sheet stiffeners, 01001
torsional buckling load including effect of skin-rib jointing method, 01001
torsional buckling load, machined or rolled sheet stiffeners, 01001
torsional-flexural buckling load including effect of skin-rib jointing method, 01001
torsional-flexural buckling load, machined or rolled sheet stiffeners, 01001
Flat Parallelogram Panels
Under Compression (Uniaxial)
buckling stress, 72012, STRUCT 02.01.47
Flat Parallelogram Plates
Under Compression (Uniaxial)
buckling stress for clamped edges, 72012, STRUCT 02.01.46
Flat Plates
Aerodynamic and Flow Characteristics
see
Boundary Layer
Boundary Walls and Fences
Centre of Pressure
Hoardings (Elevated Above Ground Level)
Normal Force
Orifices
Perforated Plates
Pressure Distribution
Skin Friction Drag
Wave Drag
Heat Transfer
see
Equilibrium Surface Temperature
Flat Rectangular Heated Plates
Forced Convection Heat Transfer
Free Convection Heat Transfer
Radiation Heat Transfer
Stress Analysis
see also
Flat Circular Plates
Flat Panels in General
Flat Parallelogram Plates
Flat Plates Tapered in Plan
Flat Rectangular Heated Plates
Flat Rectangular Plates
Flat Rectangular Plates Tapered in Thickness
Flat Specially-orthotropic Rectangular Plates
Flat Specially-orthotropic Square Plates
Flat Square Plates
Flat Square Plates with Central Circular Hole
Flat Square Plates with Central Flanged Circular Hole
Flat Strips of Isotropic Materials
Flat Strips of Orthotropic Materials
Flat Triangular Plates
Flat Unbalanced Laminated Rectangular Plates
Laminated Construction Using Composites
Stresses At Free Edges
Stress Concentration in
see
Adjacent Circular Holes in Flat Plates
Circular Holes in Bars or Strips
Circular Holes in Flat Plates
Circular Holes in Orthotropic Plates
Countersunk Holes
Elliptical Holes in Flat Plates
Fillets in Bars or Strips
Notches with Flat Bottoms in Bars or Strips
Notches with Flat Bottoms in Edge of Plate
Rectangular Holes in Flat Plates
Reinforced Circular Holes in Flat Plates
Reinforced Circular Holes Near Edge of Flat Plates
Reinforced Elliptical Holes in Flat Plates
Reinforced Square Holes with Rounded Corners in Flat Plates
Reinforced Triangular Holes in Flat Plates
Slots in Bars or Strips
Square Holes with Rounded Corners in Flat Plates
Stress Concentration
Triangular Holes with Rounded Corners in Flat Plates
U-notches in Bars or Strips
U-notches in Edge of Plate
Stress Intensity Factors
see
Stress Intensity Factors
Stress Response to Acoustic Loading
see
Flat Panels in General
Flat Sandwich Panels (Cores of Negligible Flexural Stiffness)
Flat Specially-orthotropic Rectangular Plates
Vibration
see
Flat Panels in General
Flat Rectangular Plates
Flat Sandwich Panels (Cores of Negligible Flexural Stiffness)
Flat Specially-orthotropic Rectangular Plates
Flat Specially-orthotropic Square Plates
Flat Square Plates
Flat Square Plates
Response of Lightweight Structures
Flat Plates Tapered in Plan
Under Compression (Uniaxial)
buckling stress for various edge conditions, 72012, STRUCT 02.01.48
Flat Rectangular Heated Plates
Heat Transfer Through
conversion factors Conversion Factors (S)
definitions and equations, 89022
Introduction to Methods of Calculating Stress and Temperature Distributions, 89021
Recovery Temperature Suddenly Increased
temperature distribution, 89026
Recovery Temperature Varying Linearly With Time
resultant forces for completely restrained edges, 89024
resultant moments for completely restrained edges, 89024
temperature distribution, 89023
thermal stresses (in heated and insulated surfaces) for free edges, 89025
Under Compression (Uniaxial, Non-Uniform)
buckling stress for various edge conditions, 69003
Under Compression (Uniaxial, Non-Uniform) With Shear
buckling stress for various edge conditions, 70002
Flat Rectangular Plates
see also
Flat Panels in General
Flat Plates
Flat Rectangular Heated Plates
Flat Rectangular Plates Tapered in Thickness
Flat Specially-orthotropic Rectangular Plates
Flat Specially-orthotropic Square Plates
Flat Square Plates
Flat Square Plates with Central Circular Hole
Flat Square Plates with Central Flanged Circular Hole
Flat Strips of Isotropic Materials
Flat Strips of Orthotropic Materials
Flat Unbalanced Laminated Rectangular Plates
Laminated Construction Using Composites
Rectangular Plates
Square Plates
Aerodynamic and Flow Characteristics
see
Boundary Walls and Fences
Centre of Pressure
Hoardings (Elevated Above Ground Level)
Normal Force
Computer Program for Buckling Stresses Under Various Loads
clamped or simply-supported edges or two edges clamped/two simply-supported, 94005
Dynamic Response for Various Edge Conditions
natural frequencies, program for uniform in-plane loading with/without shear, 90016, TM 71
natural frequencies, uniform biaxial or uniaxial loading, 75030
Dynamic Response to Excitation
see also
Response of Lightweight Structures
equation for coupling loss factor for connected, 98020, 99009
equation for modal density in bending, 99009
estimation of edge rotation restraint from known resonance frequencies, 00002
use of principle of reciprocity to estimate from kown radiation efficiency, 00002
Estimation of Radiation Efficiency When Dynamically Excited
simply-supported edges with edge rotation restraint, 00002
Triangular Plates, 09013
Under Bending (Edgewise)
buckling stress, simply-supported edges, 88034, STRUCT 02.04.04
Under Compression-and-Tension (Biaxial or Uniaxial) With Shear
buckling stress, clamped or simply-supported edges, 94005
buckling stress, two edges clamped and two simply-supported, 94005
Under Compression-and-Tension (Biaxial, Uniform)
buckling stress, clamped or simply-supported edges, 72012, 72019, 81047, 88034, 94005
buckling stress, two edges clamped and two simply-supported, 72012, 72019, 81047, 88034, 94005
introduction and description of effect of initial irregularities on buckling, 72012
natural frequencies for various edge conditions, 75030
plasticity effects on buckling stress, 72012, 72019, 83044
program for natural frequencies for various edge conditions, 90016, TM 71
Under Compression (Biaxial or Uniaxial, Uniform)
approximate buckling stress for various edge conditions, 75030
buckling stress, clamped or simply-supported edges, 72012, 72019, 81047, 88034, 94005
buckling stress, two edges clamped and two simply-supported, 72012, 72019, 81047, 88034, 94005
introduction and description of effect of initial irregularities on buckling, 72012
natural frequencies for various edge conditions, 75030
plasticity effects on buckling stress, 72012, 72019, 83044
program for natural frequencies for various edge conditions, 90016, TM 71
Under Compression (Biaxial or Uniaxial, Uniform) With Shear
buckling stress, clamped or simply-supported edges, 81047, 94005
buckling stress, two edges clamped and two simply-supported, 81047, 94005
program for natural frequencies for various edge conditions, 90016, TM 71
Under Compression (Uniaxial, Linearly Varying)
buckling stress, simply-supported edges, STRUCT 02.04.04
Under Compression (Uniaxial, Linearly Varying) With Shear
buckling stress, simply-supported edges, STRUCT 02.04.05
Under Compression (Uniaxial, Non-Uniform)
buckling stress for various edge conditions, 69003
Under Compression (Uniaxial, Non-Uniform) With Shear
buckling stress for various edge conditions, 70002
Under Compression (Uniaxial, Uniform)
average and edge stresses for various edge conditions, STRUCT 02.01.02, STRUCT 02.01.23
average and edge stresses for various edge conditions, aluminium alloy, STRUCT 02.01.03
buckling stress for edges held against antisymmetric rotation, STRUCT 02.01.22
buckling stress for various edge conditions, 72012, 72019, 81047, 94005
Under Compression (Uniaxial, Uniform) With Shear
average and edge stresses for simply-supported edges, STRUCT 02.04.02
buckling stress, clamped or simply-supported edges, 81047, 94005, STRUCT 02.04.01
buckling stress for various edge conditions, STRUCT 02.04.01
buckling stress, two edges clamped and two simply-supported, 81047, 94005, STRUCT 02.04.01
program for natural frequencies for various edge conditions, 90016, TM 71
Under Normal Pressure (Linearly Varying)
deflections for various edge conditions, 69018
stresses for various edge conditions, 69018
Under Normal Pressure (Uniform)
deflections, stresses and strains for various edge condition, 93011, 94033
effect of edge reinforcement on stresses, 67029
in-plane moments and forces for various edge conditions, 93011, 94033
Under Shear
buckling stress, clamped or simply-supported edges, 71005, 81047, 88034, 94005
buckling stress for various edge conditions, 71005
buckling stress, two edges clamped and two simply-supported, 71005, 81047, 88034, 94005
plasticity effects on buckling stress, 71005, 83044
program for natural frequencies for various edge conditions, 90016, TM 71
Flat Rectangular Plates Tapered in Thickness
Under Compression (Uniaxial, Uniform)
buckling stress for various edge conditions, 72012, STRUCT 02.01.49
Flat Sandwich Panels (Cores of Negligible Flexural Stiffness)
see also
Faceplate Wrinkling
Noise
Sandwich Panels and Plates
Damping Ratio Values
typical values, 91012
variation with frequency, 73011
Experimental Method of Determining Flexural Stiffness, 66025
Introduction to Data Items on, 68029
Moduli of Rigidity of Panels With Honeycomb Cores, 67022
Program for Buckling Stresses Under Various Loads
clamped or simply-supported edges, 81047, 94005
two edges clamped and two simply-supported, 81047, 94005
Transverse (Through-Thickness) Shear Stiffness
experimental method of determination, 66025
program to compute, 89013
values for panels with honeycomb core, 67022
Under Compression-and-Tension (Biaxial)
overall buckling load, clamped edges, 68031, 81047, 94005
overall buckling load, simply-supported edges, 67025, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression-and-Tension (Biaxial) With Shear
overall buckling load, clamped or simply-supported edges, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Biaxial or Uniaxial)
overall buckling load, clamped edges, 68031, 81047, 94005
overall buckling load, simply-supported edges, 67025, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Biaxial or Uniaxial) With Shear
overall buckling load, clamped or simply-supported edges, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Uniaxial)
choice of core material, 75006
effect of core and faceplate properties on buckling, 75006
minimum weight design (with plasticity and dimensional restriction), 75006
Under Normal Pressure (Uniform)
deflections and stresses, all edges clamped, 77003
deflections and stresses, all edges simply-supported, 76013
deflections and stresses, long edges clamped and short edges simply-supported, 76022
Under Shear
overall buckling load, clamped edges, 68030, 81047, 94005
overall buckling load, simply-supported edges, 67024, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
With Isotropic Faceplates
natural frequencies, 72016
With Isotropic Faceplates Under Acoustic Loading
effect of bevelled edge on ratio of surface strains at centre, 95026
effect of bevelled edge on strain at mid-point of longer side, 95026
stress response at centre neglecting edge effects, 72017
With Orthotropic (Laminated Composite) Faceplates
program for lower natural frequencies (bending modes), 86024
With Orthotropic (Laminated Composite) Faceplates Under Acoustic Loading
program for strain response at centre on surfaces in orthogonal directions, 86024
Flat Sandwich Panels (Corrugated Cores)
see also
Noise
Sandwich Panels and Plates
Flexural Stiffness
experimental method of determination, 66025
Introduction to Data Items on, 68029
Program for Buckling Stresses Under Various Loads
clamped edges or simply-supported edges or two edges clamped and two simply-supported, 81047, 94005
Transverse (Through-Thickness) Shear Stiffness
experimental method of determination, 66025
program to compute, 89013
values for equal faceplates, STRUCT 07.03.01
Under Compression-and-Tension (Biaxial)
overall buckling load, clamped edges, 68033, 81047, 94005
overall buckling load, simply-supported edges, 67032, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression-and-Tension (Biaxial) With Shear
overall buckling load, clamped or simply-supported edges, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Biaxial or Uniaxial)
overall buckling load, clamped edges, 68033, 81047, 94005
overall buckling load, simply-supported edges, 67032, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Biaxial or Uniaxial) With Shear
overall buckling load, clamped or simply-supported edges, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Under Compression (Uniaxial)
local and overall buckling load including effect of bonding adhesive layer, 98016
local buckling stress, 68037, STRUCT 02.01.37
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of adhesive bonding layer, 01001
Under Shear
overall buckling load, clamped edges, 68032, 81047, 94005
overall buckling load, simply-supported edges, 67026, 81047, 94005
overall buckling load, two edges clamped and two simply-supported, 81047, 94005
Flat Sandwich Panels (Isotropic Cores)
Under Compression (Uniaxial)
local and overall buckling load including effect of bonding layer, 98016
Under Compression (Uniaxial) Taking Account of Plasticity
local and overall buckling load including effect of adhesive bonding layer, 01001
Flat Sandwich Panels (Truss Cores)
see also
Flat Sandwich Panels (Corrugated Cores)
Sandwich Panels and Plates
Flexural Stiffness
experimental method of determination, 66025
Introduction to Data Items on, 68029
Tranverse (Through-Thickness) Shear Stiffness
experimental method of determination, 66025
program to compute, 89013
Under Compression-and-Tension (Biaxial)
overall buckling load for various edge conditions, 81047, 94005
Under Compression-and-Tension (Biaxial) With Shear
overall buckling load for various edge conditions, 81047, 94005
Under Compression (Biaxial or Uniaxial)
overall buckling load for various edge conditions, 81047, 94005
Under Compression (Biaxial or Uniaxial) With Shear
overall buckling load for various edge conditions, 81047, 94005
Under Compression (Uniaxial)
local buckling stress taking into account joint stiffness, 80010
Under Shear
overall buckling load for various edge conditions, 81047, 94005
Flat Specially-orthotropic Rectangular Plates
see also
Circular Holes in Orthotropic Plates
Laminated Construction Using Composites
Dynamic Response
program for natural frequencies, 83036
program for natural frequencies with any uniform in-plane loading, 90016, TM 71
Dynamic Response to Excitation
see also
Noise
program for stresses due to acoustic loading, 84008
Program to Design Most Effective Laminate to Support In-Plane Loads and Bending Moments
choice of ply thicknesses and lay up using 0?, 90?, ?45? layers only, 96036
Under Compression-and-Tension (Biaxial)
buckling stress for various edge conditions, 80023, 81047, 94005
Under Compression-and-Tension (Biaxial) With Shear
buckling stress for various edge conditions, 80023, 81047, 94005
Under Compression (Biaxial or Uniaxial)
buckling stress for various edge conditions, 80023, 81047, 94005
Under Compression (Biaxial or Uniaxial) With Shear
buckling stress for various edge conditions, 80023, 81047, 94005
Under Normal Pressure
program for deflections for various edge conditions, 93011
program for in-plane moments and forces for various edge conditions, 93011
program for stresses and strains for various edge conditions, 93011
Under Shear
buckling stress for various edge conditions, 80023, 81047, 94005
Flat Specially-orthotropic Square Plates
see also
Flat Specially-orthotropic Rectangular Plates
Dynamic Response to Excitation
program for natural frequencies with any uniform in-plane loading, 90016, TM 71
Under Normal Pressure
program for deflections for various edge conditions, 93011
program for in-plane moments and forces for various edge conditions, 93011
program for stresses and strains for various edge conditions, 93011
Flat Square Plates
see also
Flat Plates
Flat Rectangular Plates
Square Plates
Dynamic Response to Excitation
estimation of edge rotation restraint from known resonance frequencies, 00002
program for natural frequencies with any uniform in-plane loading, 90016, TM 71
use of principle of reciprocity to estimate from known radiation efficiency, 00002
Estimation of Radiation Efficiency When Dynamically Excited
simply-supported edges with edge rotation restraint, 00002
Under Normal Pressure
deflections and stresses for various edge conditions by graphical method, 70001
program for deflections for various edge conditions, 93011, 94033
program for in-plane moments and forces for various edge conditions, 93011, 94033
program for stresses and strains for various edge conditions, 93011, 94033
Flat Square Plates with Central Circular Hole
Under Shear
initial buckling stress and maximum direct stress, 75034
overall shear strain, 75034
Flat Square Plates with Central Flanged Circular Hole
Under Shear
initial buckling stress for various flange forms, 75035
Flat Strips of Isotropic Materials
Stress Concentration in
see
Circular Holes in Bars or Strips
Fillets in Bars or Strips
Notches with Flat Bottoms in Bars or Strips
Slots in Bars or Strips
U-notches in Bars or Strips
Under Compression (Biaxial) With Sinusoidally Distributed Edge Couples
stiffness, 73007, STRUCT 02.01.28
Under Shear
plasticity correction factors for various edge conditions, 83044
Under Uniaxial Compression
plasticity correction factors for various edge conditions, 83044
Flat Strips of Orthotropic Materials
see also
Laminated Construction Using Composites
Under Compression (Biaxial) With Sinusoidally Distributed Edge Couples
stiffness, 73007, STRUCT 02.01.28
Flat Triangular Plates
see also
Flat Plates
Triangular Plates
Under Compression (Two Edges Clamped or Simply-Supported)
buckling stress of free edge, 88034
Under Compression (Uniform) With Shear (Simply-Supported Edges)
buckling stress, 09013
Flat Unbalanced Laminated Rectangular Plates
see also
Laminated Construction Using Composites
Noise
Program for Lower Natural Frequencies
with uniform in-plane biaxial loading, 89011
Under Compression-and-Tension (Biaxial)
buckling stress, simply-supported edges, 94006
Under Compression (Biaxial or Uniaxial)
buckling stress, simply-supported edges, 94006
Flaw Detection
see
Non-destructive Examination

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