cast.config

Classes

cast.config.Engine

class cast.config.Engine

ENGINE Summary of this class goes here Detailed explanation goes here

Constructor Summary

Engine(T_Static, L, D, M, SFC_TO, SFC_cruise, BPR, alt_cruise, M_cruise)

Property Summary

BPR

Diameter

Length

Mass

SFC_A

SFC_B

SFC_TO

SFC_cruise

T_Static

Method Summary

static CFM56_5(): CFM56_5 Data for CFM56-5 as on a318/a319 https://en.wikipedia.org/wiki/CFM_International_CFM56

static CFM_LEAP_1A(sfc_scaling, alt_cruise, M_cruise)

Rubberise(T_new)

TSFC(M, alt)

cast.config.Fuel

class cast.config.Fuel

ENGINE Summary of this class goes here Detailed explanation goes here

Constructor Summary

Fuel(Name, SpecificEnergy, CostPerKilo, Density)

Property Summary

CostPerKilo

Density

Name

SpecificEnergy

Method Summary

static JA1(): Jet A1

static LH2(): Liquid Hydrogen

cast.config.TAW

class cast.config.TAW

Bases: cast.ADP

TAW Summary of this class goes here Detailed explanation goes here

Constructor Summary

TAW()

Property Summary

Baff

CD0_meta

Dihedral

Engine

Masses

TrappedFuel

Method Summary

AdjustCoM(p): AdjustCoM adjust wing pos to get CoM at OEM at p % of MAC

AdjustCoM_NP(p): AdjustCoM_NP adjust wing pos to get CoM at OEM at p % in front of NP THIS HAS A BUG - it assumes tail is as effective and wing…

BuildBaff(opts)

BuildWing(isRight, D_c, HasFuel, opts)

ConstraintAnalysis(opts)

EstimateOswald(Mach, Method)

GetNeutralPoint()

MJperPAX(range, payloadFactor, opts)

MissionAnalysis(opts)

NitaOswald(Mach): NITAOSWALD uses method from “Estimating the Oswald factor from Basic Aircraft Geometrical Paramters” to estimate oswald efficency factor of a Baff Aircraft

PR_diagram()

PrintMass()

ToMeta()

UpdateAeroEstimates(): UPDATEAEROESTIMATES Summary of this function goes here Detailed explanation goes here