ESDU A-Z Index: FLAT-FLD
- see also
- Circular Plates
- Flat Plates
- Under Normal Pressure
- stresses and large deflections for various edge conditions, 65003
- see
- Disc Springs
- 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
- 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
- see also
- Flat Panels in General
- Under Compression (Biaxial)
- local buckling stress, 73015
- 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
- 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
- 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
- see also
- Flat Panels in General
- Under Shear
- buckling stress, STRUCT 02.03.02
- 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
- 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
- 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
- Under Compression (Uniaxial)
- buckling stress, 72012, STRUCT 02.01.47
- Under Compression (Uniaxial)
- buckling stress for clamped edges, 72012, STRUCT 02.01.46
- Aerodynamic and Flow Characteristics
- 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
- Stress Response to Acoustic Loading
- Vibration
- Under Compression (Uniaxial)
- buckling stress for various edge conditions, 72012, STRUCT 02.01.48
- 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
- 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
- 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 known 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
- Under Compression (Uniaxial, Uniform)
- buckling stress for various edge conditions, 72012, STRUCT 02.01.49
- 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
- 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
- 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
- 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
- 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
- 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
- Under Shear
- initial buckling stress for various flange forms, 75035
- Stress Concentration in
- 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
- Under Compression (Biaxial) With Sinusoidally Distributed Edge Couples
- stiffness, 73007, STRUCT 02.01.28
- see also
- Flat Plates
- Triangular Plates