cast

Subpackages

Classes

cast.ADP

class cast.ADP

Bases: handle

ADP Aircraft Design Parameters

Constructor Summary

ADP()

Property Summary

ADR: Aircraft Design Requirements

AR

CD0

CD_LDG: CD in ground run on landing

CD_TO: CD in ground run

CL_LDG: CL during ground run on landing

CL_TO: CL during ground run

CL_TOmax: max CL in TO condition

CL_cruise: CL during cruise

CL_max: Max CL in landing configuration

Cl_max: airfoil amx Cl for wing

Delta_Cl_ld

Delta_Cl_to

EngineEta

FuelType

KinkEta

LD_app

LD_c

MTOM

Mf_Fuel: mass ratio fuel

Mf_Ldg: mass ratio at landing

Mf_TOC: mass ratio top of climb

Mf_res: Resevre Fuel ratio

N_eng

OEM

SFC_0: specific fuel consumption on ground

SFC_app: specific fuel consumption on ground

SFC_c: SFC cruise

Span

TW_idle

TWgr: thrust to weight ratio on ground run

Thrust

V_HT: Horizontal Tail Volume

V_VT: Vertical tail volume

WingArea

WingEta

WingletHeight

e: Oswald Efficency Factor

Method Summary

Clone()

cast.ADR

class cast.ADR

ADP Aircraft Design Requirements

Property Summary

Alt_alternate

Alt_cruise

Alt_max: max altitude in m

Crew

CrewMass

ExtraPayload

GroundRun

GroundRunLanding

Loiter: 30 minutes in seconds

M_alt: Mach number at each alititude to be limited by either M_c or V_climb

M_c: cruise Mach number

PAX

Payload

Range

Range_alternate

V_app: approach speed

V_climb: climb speed (CAS)

Method Summary

static A320(PAX, Range, TargetPayload)

cast.LoadCase

class cast.LoadCase

LOADCASE Summary of this class goes here Detailed explanation goes here

Property Summary

Alt

ConfigParams

IdxOverride: if not nan overrides idx of load case

LoadFactor

Mach

Name

Nonlinear

SafetyFactor

Type

Method Summary

static Dummy()

static Ground(opts)

static Gust(Mach, alt, opts)

static Manoeuvre(Mach, alt, LoadFactor, opts)

static Turbulence(Mach, alt, opts)

cast.Masses

class cast.Masses

MASSES Summary of this class goes here Detailed explanation goes here

Constructor Summary

Masses(inputArg1, inputArg2): MASSES Construct an instance of this class Detailed explanation goes here

Property Summary

Fuselage

Wing

Method Summary

method1(inputArg): METHOD1 Summary of this method goes here Detailed explanation goes here

cast.Meta

class cast.Meta

META Summary of this class goes here Detailed explanation goes here

Property Summary

Alt_cruise

Alt_max: max altitude in m

AspectRatio

CD0

CL_c

CostPerKilo

Crew

Fuel_block

Fuel_capacity

Fuel_trip

FuselageRadius

HingeEta

LD_c: Aero

Length

MFRES

MLND

MTOM

MZFM

M_c: cruise Mach number

OEM

PAX: paylaod

Payload

Payload_asym

Range_Design

Range_asym

Range_ferry

Range_harm

Span

SpecificEnergy

Thrust

WingArea

e

Method Summary

PrintInfo()

PrintNames()

cast.Mission

class cast.Mission

MISSION Summary of this class goes here Detailed explanation goes here

Constructor Summary

Mission()

Property Summary

Segments

Method Summary

static StandardWithAlternate(ADR, Range)

cast.SI

class cast.SI

SI Summary of this class goes here Detailed explanation goes here

Property Summary

DragCount

FL: Flight Level (hundreds of feet)

Nmile

Tonne

bar

ft

gal

hr

inch

km

knt

lb

lbf

lbft

litre

mile

min

psi