cast.size

Classes

cast.size.AbstractLoads

class cast.size.AbstractLoads: Bases: handle

cast.size.BaffSizing

class cast.size.BaffSizing

Bases: handle

AircraftSizing Summary of this class goes here Detailed explanation goes here

Property Summary

Baff: baff model

LoadsSurrogate

Name

RibPitch

Tags

WingBoxParams

size

Method Summary

ApplyWingParams(Par)

ExtractMeta(filename)

SetupWings()

StructuralSizing(Cases, opts)

cast.size.Loads

class cast.size.Loads

LOADS Summary of this class goes here Detailed explanation goes here

Constructor Summary

Loads(N, opts)

Property Summary

Fx

FxIdx

Fy

FyIdx

Fz

FzIdx

IDs

Meta

Mx

MxIdx: Name of critical load case

My

MyIdx

Mz

MzIdx

t: time for dyanmic loads

Method Summary

IncreaseIdx(val)

SetIdx(id)

abs()

and(obj2)

max()

min()

minus(obj2)

or(obj2)

plot(load, Params, opts)

plus(obj2)

repmat(n)

times(val)

cast.size.NullLoads

class cast.size.NullLoads

Bases: cast.size.AbstractLoads

Method Summary

GetLoads(Cases)

SetConfiguration(opts)

cast.size.RibParams

class cast.size.RibParams

Constructor Summary

RibParams(Span, Pitch)

Property Summary

ActualPitch: distance in y between each rib

Eta: Normalised Position of each Rib

IdealPitch: Specified rib pitch

Min_Thickness

NumEl: Number of Ribs

Span

Thickness: Thickness of each rob

Method Summary

apply(obj2): wings can have diffetn numbers of ribs so we need to interpolate again

combine(obj2)

interpolate(etas)

minus(obj2)

plus(obj2)

rdivide(val)

times(val)

cast.size.SkinParams

class cast.size.SkinParams

SKINPARAMS Summary of this class goes here Detailed explanation goes here

Constructor Summary

SkinParams(NumEl, Span, opts): SKINPARAMS Construct an instance of this class Detailed explanation goes here

Property Summary

Effective_Width

Eta

NumEl

Skin_Min_Thickness: minimium values

Skin_Thickness

Span

StrgFlange_Width

StrgGround_Width

StrgThickness_Flange

StrgThickness_Ground

StrgThickness_Web

Strg_Depth

Strg_Min_Thickness

Strg_Pitch

Method Summary

apply(obj2)

combine(obj2)

interpolate(etas): METHOD1 Summary of this method goes here Detailed explanation goes here

minus(obj2)

plus(obj2)

rdivide(val)

times(val)

cast.size.WingBoxSizing

class cast.size.WingBoxSizing

WINGPARAMS Summary of this class goes here Detailed explanation goes here

Constructor Summary

WingBoxSizing(NumEl, Span, Mat, opts)

Property Summary

CapEta_height

CapEta_width: spar properties

Eta

Height

Index

Mat: Material

Name

NumEl

Ribs: Ribs

Skin: skin-stringer panels

Span

SparCap_Thickness

SparWeb_Stiff_N: Number of Stiffeners on web

SparWeb_Stiff_Thickness: Thickness of stiffeners

SparWeb_Thickness

Spar_Min_Thickness: minValues

Width

size

Method Summary

Area(): Shorthand variables

BeamCondensation()

GetMass()

GetSpanwiseMass()

Iyy(): Shorthand variables

Izz(): Shorthand variables

J(): Shorthand variables

Size(Loads, SafetyFactor, opts)

SizeStep(Loads, SafetyFactor)

apply(params)

combine(obj2)

eq(obj1, obj2)

interpolate(etas): return a new WingBoxSizing object with interpolated values

minus(obj2)

mtimes(val)

plus(obj2)

rdivide(val)

times(val)