Zones are panels and beams of constant cross-section that are analyzed to return margins of safety and optimum Sizing results. They are the fundamental entity in HyperX - as cross-section dimensions, materials, and failure criteria/settings are all assigned to and/or optimized for each Zone.
Important
HyperX analyzes panel and beam Zones, not finite elements. A Zone is a collection of finite elements used to represent a panel or a beam.
In the image below, a wing box is shown modeled with a panel Zone per bay. Each of these panels can have its own Sizing/Analysis results.
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HyperX panel and beam designs replace FEM properties. They provide structural detail to the model in order to find optimal lightweight concepts, dimensions, materials, and laminates while achieving positive margins to aerospace analyses methods for all load cases. Read more on the Feature Page on our main website, found here.
Elements ID selections are used to define the coverage of Zones - much like property assignment to elements works in the FEM-world. An element can only belong to one Zone at a time.
In order to be Sized and/or Analyzed:
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Zones must belong to a Structure in order to be Sized/Analyzed.
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A Design Property must be assigned to a Zone to apply corresponding design space definitions to selected Zone(s) for Sizing/Analysis.
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A Load Property must be assigned to a Zone to apply the corresponding loads processing technique to the selected Zone(s).
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An Analysis Property must be assigned to a Zone to apply the corresponding Failure Modes and their respective analysis defaults to the selected Zone(s).
Note
Zones can optionally be organized into Sets to aid with model management.
There are two primary types of Zones, delineated by the FEM element types of which they are comprised:
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Beams/1D Zones - Made up of 1-dimensional (bar) FEM elements, can only be assigned Beam (1D) Design Properties.
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Panels/2D Zones - Made up of 2-dimensional (shell) FEM elements, can only be assigned Panel(2D) Design Properties.
Note
Panel Segments can be considered a special kind of Zone corresponding to discretely stiffened panels but they are not organized in the same way as Beam and Panel Zones.
Panel Settings
The Panel Settings form can be accessed by right-clicking on the desired panel in the viewport and then selecting "Panel Settings." Any of these settings can be applied to multiple zones at once in a tabulated manner using the Zone Settings Table.
Design
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Non-optimum Factor - Used to book-keep weight that is not tracked in the panel design representation in HyperX, such as fillets or adhesive weights. The unit weight of the Zone will be scaled up by this factor.
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Added Weight - Similar to the factor above, except this unit weight value is added to the Zone unit weight. Typically used to represent features that do not scale up or down with the cross-section of the panel, such as a thermal protection system (TPS).
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Honeycomb Core Angle - Used to account for a non-zero (typically 90deg) honeycomb core angle during sandwich panel Analysis and Sizing.
Loads
Superimposed Loads
The 'superimposed loads' category holds toggles/settings options for all loads that are calculated individually and then superimposed onto the resulting panel Design-to Loads. See Superimposed Loads for a more in-depth description of this process. The settings controlled here are defined as follows:
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Panel Pressure - Toggles on/off the option to include pressure-induced out-of-plane shear and moment loads in the panel Design-to Loads for selected panel(s).
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Beam-Column - Toggles on/off the option to treat the selected panel(s) as beams for a pressure deflection calculation - thereby including additional shear and moment loads caused by the combined effect of in-plane compression and lateral deflection to the panel Design-to Loads.
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Initial Imperfection - Allows for user-defined length of initial imperfection for beam-column analysis (as opposed or in addition to pressure loading).
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Boundary Condition Drop-Down - Allows for the selection of Fixed or Simple Boundary Conditions - used to bind the Panel Pressure and Beam-Column analyses.
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Zero Curvature - If this option is enabled, all moments from the FEM will be ignored. Only the membrane loads are imported, and zero curvature boundary conditions are assumed. If this option is disabled, all load components from the FEM are imported
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Zero FEA Transverse Shear - If this option is enabled, all transverse shear (\(Q_x\) and \(Q_y\)) loads from the FEM will be ignored. Only the membrane loads and moments are imported. If this option is disabled, all load components from the FEM are imported.
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Local Pressure (for skin panels of discretely stiffened panels) - Toggles on/off the superimposition of local pressure loads on the skin segment of a stiffened panel by the stiffener loads.
FEA Load Factors
In general, user-defined load factors are used to scale up (or down) the applied load according to design specifications. Zone-specific Load Factors are applied in this panel-settings form. Any loads applied here are combined with those defined on the Design Load Case Form for all Design Load Cases for the selected panel(s).
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Mechanical Limit Applies to mechanical loads for limit margins of safety.
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Mechanical Ultimate Applies to mechanical loads for ultimate margins of safety.
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Thermal Hurt/Help Applies to thermal loads for both limit and ultimate margins of safety.
Tip
For more information on how these locally applied load factors are used, see Load Factors.
Reference Plane
The selected Reference Plane option sets the reference plane (about which loads and moments are calculated) for the selected panel(s). This will be automatically determined during FEM Import based on element reference planes and normal directions. See Shell Reference Planes and Offsets. However, the user can change them here. Use figures below for reference.
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Top Face Midplane - The shell offset is located at the midplane of the top facesheet or top stack.
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Midplane - The shell offset is exported at the midplane of the entire stack.
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Bottom Face Midplane - The shell offset is exported at the midplane of the bottom facesheet or bottom stack.
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Top - The shell offset is exported at the top of the entire stack. If element normal directions are pointed outward, this is equivalent to OML offset.
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Bottom - The shell offset is exported at the bottom of the entire stack. If element normal directions are pointed outward, this is equivalent to IML offset.
Buckling
All panel settings that apply to HyperX-native analytical buckling methods can be found under the 'Buckling' heading.
Geometry and Boundary Conditions
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Buckling Spans (X Span, Y Span) - Dialog boxes contain the X Span (length) and Y Span (width) of the panel. When panels are placed into Structures, buckling spans will be automatically derived for each panel. See Buckling Span Calculations. The user also has the ability to overwrite these values manually if necessary.
Buckling spans can be plotted directly on the visible panels from the View tab of the Ribbon.
Impact of Buckling Spans on Analysis Methodologies:
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Panel and Beam Buckling Failure Criteria - Buckling spans drive overall buckling modes for all panel and beam buckling analyses. See Panel Buckling, Beam Buckling, and Flexural-Torsional Buckling.
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Local Buckling Failure Criteria - Mathematically, the buckling spans will always affect the local buckling analysis. However, this effect is usually negligible - except in cases in which the beam is relatively short. See Local Buckling.
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Beam-Column Loading - The length of the panel or beam is a key driver in the beam-column analysis option. See the Beam-Column section of the Superimposed Loads page.
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Panel Pressure Loading - A larger panel or beam (i.e. greater x and y buckling spans) will experience an increase in deflection due to pressure. See the Panel Pressure section of the Superimposed Loads page.
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Primary Stress - (\(N_x\), \(N_y\), \(N_{xy}\), \(M_x\), \(M_y\), \(M_{xy}\), \(Q_x\), and \(Q_y\)) - panel buckling span definitions do not impact the primary stress analysis in any way. This analysis only considers a single repeating unit of the stiffener and skin. No length dimension is considered.
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Curvature - The curvature options are used to set the orientation and radius of a curved panel. If the 'Component is Full Cylinder' check box is enabled, the transverse span is set to the full circumference. If the panel is curved, panel pressure is ignored. However, local pressure is still applied.
Panel pressure is ignored for curved panels - as the pressure load is assumed to be reacted in the hoop direction (\(N_y\)). During FEM import, HyperX will attempt to define whether or not a given panel is curved, as well as the direction of curvature. These initial settings can be overwritten manually by the user for any panel at any time. See the images below for reference.
Post-Buckling
'Checking' the Local Postbuckling option enables the postbuckling analyses outlined here: Postbuckling.
Constraints
The 'Required Stiffness' category holds dialog boxes to allow for user-input required stiffness values. There is one box for each respective stiffness component or derivative value, all of which correspond to their own Failure Criteria. See Required Stiffness for a more in-depth description of this process.
Beam Settings
The Beam Settings form can be accessed by right-clicking on the desired beam in the Viewport and then selecting "Beam Settings." Any of these settings can be applied to multiple Zones at once in a tabulated manner using the Zone Settings Table.
Design Settings
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Non-optimum Factor - Used to book-keep weight that is not tracked in the beam design representation in HyperX, such as fillets or adhesive weights. The unit weight of the Zone will be scaled up by this factor.
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Added Weight - Similar to the factor above, except this unit weight value is added to the Zone unit weight. Typically used to represent features that do not scale up or down with the cross-section of the beam, such as a thermal protection system (TPS).
Load Settings
Superimposed Loads
The 'Superimpose loads' category holds toggles/settings options for all loads that are calculated individually and then superimposed onto the resulting beam design-to loads. See Superimposed Loads for a more in-depth description of this process. The settings controlled here are defined as follows:
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Beam Distributed Load - Toggles on/off the option to account for distributed pressure loads applied to the beam in the FEM, in addition to the primary beam-theory loads
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Beam-Column - Toggles on/off the option to apply a pressure deflection calculation to selected beams - thereby including additional shear and moment loads caused by the combined effect of in-plane compression and lateral deflection to the beam design-to loads.
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Initial Imperfection - Allows for the user-defined length of initial imperfection for beam-column analysis (as opposed to or in addition to pressure loading)
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Zero Curvature - If this option is enabled, all moments from the FEM will be ignored. Only the membrane loads are imported and zero curvature boundary conditions are assumed. If this option is disabled, all load components from the FEM are imported
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Zero FEA Transverse Shears - If this option is enabled, all transverse shear (\(Q_x\) and \(Q_y\)) loads from the FEM will be ignored. Only the membrane loads and moments are imported. If this option is disabled, all load components from the FEM are imported.
FEA Load Factors
In general, user-defined load factors are used to scale up (or down) the applied load according to design specifications. Zone-specific load factors are applied in this beam-settings form. Any loads applied here are combined with those defined on the Design Load Case Form for all design load cases for the selected beam(s).
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Mechanical Limit Applies to mechanical loads for limit margins of safety.
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Mechanical Ultimate Applies to mechanical loads for ultimate margins of safety.
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Thermal Hurt/Help Applies to thermal loads for both limit and ultimate margins of safety.
Tip
For more information on how these locally-applied load factors are used, see Load Factors.
Reference Plane
The selected Reference Plane option sets the reference plane (about which loads and moments are calculated) for the selected beam(s).
Buckling
All beam settings that apply to HyperX-native analytical buckling methods can be found under the 'Buckling' heading.
Geometry and Boundary Conditions
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Boundary Conditions - Contains assumed beam buckling boundary conditions, used as primary assumptions for analytical buckling solutions. These can be changed for each beam end individually using the dropdown menu pertaining to each edge (HyperX coordinates).
Note
These boundary conditions do not affect the overall stress analysis or local buckling margins in the beam. They only serve to guide the analytical buckling solutions.
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Buckling Spans (X Span) - The dialog box contains the X Span (length) of the beam. During FEM Import, buckling spans will be automatically derived for each beam. The user also has the ability to overwrite these values manually if necessary. Buckling spans can be plotted directly on the visible beams from the tab of the Ribbon.
Impact of Buckling Spans on Methodologies:
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Panel and Beam Buckling Failure Criteria - Buckling spans drive overall buckling modes for all panel and beam buckling analyses. See Panel Buckling, Beam Buckling, and Flexural-Torsional Buckling.
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Local Buckling Failure Criteria - Mathematically, the buckling spans will always affect the local buckling analysis. However, this effect is usually negligible - except in cases in which the beam is relatively short. See Local Buckling.
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Beam-Column Loading - The length of the panel or beam is a key driver in the beam-column analysis option. See the Beam-Column section of the Superimposed Loads page.
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Panel Pressure Loading - A larger panel or beam (i.e. greater x and y buckling spans) will experience an increase in deflection due to pressure. See the Panel Pressure section of the Superimposed Loads page.
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Primary Stress - (\(N_x\), \(N_y\), \(N_{xy}\), \(M_x\), \(M_y\), \(M_{xy}\), \(Q_x\), and \(Q_y\)) - panel buckling span definitions do not impact the primary stress analysis in any way. This analysis only considers a single repeating unit of the stiffener and skin. No length dimension is considered.
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Knockdown Factors
"Knockdown factors" can be entered for the local buckling analysis. These factors are traditionally used in the aerospace industry to account for initial imperfections and uncertainties in panels and beams. Entering a factor between 0 and 1 will "knockdown" the allowable buckling load by this factor (i.e. a factor of 0.8 will reduce the calculated allowable buckling load by 20%).
Post-Buckling
'Checking' the Local Postbuckling option enables the postbuckling analyses outlined here: Postbuckling.
Required Stiffness Constraints
The 'Required Stiffness' category holds dialog boxes to allow for user-input required stiffness values. There is one box for each respective stiffness component or derivative value, all of which correspond to their own Failure Criteria. See Required Stiffness for a more in-depth description of this process.
Zone Settings Table
The Zone Settings Table contains all of the settings found on the Panel Settings and Beam Settings menus presented in a tabular format. This form is useful for viewing or modifying the settings on many Zones at once. The table can be accessed by either right-clicking on Zones in the Viewport, or from the button in the "Edit Zones" group of the Structures tab on the Ribbon.
The "find and replace" button on the top-left of the form can be used to quickly change data in multiple cells. The tools on the top-right of form can be used to hide or show columns, as well as create a data template with the current hidden/shown state of columns.
Two methods for creating Zones are described below.
Option #1: From the FEM Tree
Zones are created automatically during Structure creation according to FEM property coverage. Each selected FEM property will be converted into a Zone entity. See Create Structures.
Option #2: By Selecting Elements in a Structure
Zones can be created by manually selecting elements in a Structure. This operation is launched from the Structure tab of the Ribbon. The specific button is indicated in the image below.
Important
Elements must already be in a Structure in order to be selected for Zone definition. This operation cannot be done on the unused FEM.
Tip
See Sizing vs. Analysis for recent updates to the Sizing and Analysis workflows.
All Zones - whether they be panels or beams - are sized by following the basic steps.
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Tell HyperX what you'd like to size.
The first step is to Import a FEM. During this process, HyperX will recognize all property cards (NASTRAN/Optistruct) or Section Definitions (Abaqus) as individual analysis entities. However, these entities are only considered Zones - and therefore can only be Sized - if they have been grouped into a Structure. See Create Structures.
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Define the design space for each Zone.
All design space inputs are applied via Design Property. First, Design Properties should be created (see 'Create Design Properties'). Then they should be assigned to their respective Zones (see 'Assign Design Properties'). When selecting and defining a Design Property, the two most consequential decisions are:
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Concept - what cross-section would you like your zone to be? Note that panels and beams have their own respective concept options. See: Panel and Beam Design Properties
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Sizing Mode - What sizing strategy will HyperX use to evaluate your zones? See: Sizing Modes
Sizing is implemented by selecting a Sizing Mode and filling out the corresponding variable definitions. Sizing inputs are treated separately from Analysis inputs - even though they can be defined on the same Design Property.
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Define the loads for each Zone. This requires two parts:
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Define the load scenarios that will be assessed. This is done by creating:
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-- AND / OR --
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Define how the element-by-element forces (for each Design Load Case) are processed into a set of Design-to Loads.
The FEA Loads Processing Technique is selected and assigned to desired zones via Load Property
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What methods am I sizing to?
HyperX offers 100s of native failure criteria for sizing and analyzing your structure. Individual methods and their corresponding settings are defined in Failure Modes. Failure Modes are then collected and assigned to selected Zones via Analysis Property.
Company-or-program-specific methods that are not implemented natively in HyperX can be added to the framework via Analysis Plugin. They can then be used alongside native methods within the Failure Mode/Analysis Property paradigm.
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Select the zones you'd like to size, and click 'Size'
Tip
See Sizing vs. Analysis for recent updates to the Sizing and Analysis workflows.
All Zones - whether they be panels or beams - are analyzed by following the basic steps.
-
Tell HyperX what you'd like to analyze.
The first step is to Import a FEM. During this process, HyperX will recognize all property cards (NASTRAN/Optistruct) or Section Definitions (Abaqus) as individual analysis entities. However, these entities are only considered Zones- and therefore can only be Analyzed - if they have been grouped into a Structure. See Create Structures.
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Define the design space for each Zone.
All design space inputs are applied via Design Property. First, Design Properties should be created (see 'Create Design Property'). Then they should be assigned to their respective Zones (see 'Assign Design Property'). When selecting and defining a design property, the two most consequential decisions are:
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Concept - What cross-section would you like your zone to be? Note that panels and beams have their own respective concept options. See: Panel and Beam Design Properties
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Analysis Inputs - What dimension and material system should be analyzed?
Analysis is implemented by selecting the 'Analysis' radial button and filling out the corresponding dimensions. Analysis inputs are treated separately from Sizing inputs - even though they can be defined on the same Design Property.
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Define the loads for each Zone. This requires two parts:
-
Define the load scenarios that will be assessed. This is done by creating:
-
-- AND / OR --
-
-
Define how the element-by-element forces (for each Design Load Case) are processed into a set of Design-to Loads.
The FEA Loads Processing Technique is selected and assigned to desired zones via Load Property
-
-
What methods am I assessing?
HyperX offers 100s of native failure criteria for sizing and analyzing your structure. Individual methods and their corresponding settings are defined in Failure Modes. Failure Modes are then collected and assigned to selected Zones via Analysis Property.
Company-or-program-specific methods that are not implemented natively in HyperX can be added to the framework via Analysis Plugin. They can then be used alongside native methods within the Failure Mode/Analysis Property paradigm.
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Select the zones you'd like to analyze, and click 'Analyze'
Two options for deleting Zones are described below. HyperX does not edit FEM element definitions or their corresponding grid definitions. Therefore, when a Zone is 'deleted,' the associated elements are not removed from the Database but rather become unassociated with a HyperX entity (or, back in the unused FEM).
Option #1: Return to Unused FEM
This option is available in the right-click menu on a Zone (in the Viewport or Structure Tree) and is equivalent to deleting the Zone. The Zone will be removed from the Structure and reappear in the preview FEM.
Option #2: Delete a Structure
Zones within a Structure are deleted when the Structure itself is deleted.