AircraftDesign | Design an aircraft for a trajectory. |

AircraftDragDataStructures | Generates data structures for select aircraft. |

AircraftGroupMassStatement | Create a mass statement for an aircraft. |

AirlinerSeat | Generate CAD data for an airliner seat. |

AirlinerSeats | Layout airliner seats. |

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AOverAStar | A/A* computation from mach number and ratio of specific heats. |

AerodynamicShock | Compute Mach number and pressure for aerodynamics shocks. |

F100 | Gas Turbine 16th-order F100 linear model: Pratt and Whitney |

FAIR | Computes the gas constants for hydrocarbon/air mixtures. This model |

FMixedExhaustTurbofan | Function called by FZero to solve for tauTL. Only y is used by FZero. |

InletLoss | Computes the inlet loss in an aircraft engine due to shockwaves. |

JetEngineAnalysis | Jet engine analysis. You can vary up to two of the |

JetEngineDefinitions | Definitions of data. If no output arguments are specified it will |

JetEngineEfficiency | Computes the jet engine efficiency for an engine. |

JetEnginePerformance | Jet engine performance. You can vary up to two of the parameters in p. |

MachAcrossShock | Compute the Mach number across a shock. |

MachFromMassFlowParameter | Mach number from mass flow parameter. You need to enter a guess for |

MachFromPR | Computes Mach number from pressure ratio and gamma. |

MassFlow | Computes the mass flow divided by the inlet area. The code |

MassFlowParameter | Mass flow parameter. |

MassFlowParameterR | Mass flow parameter with gamma, r and Mach number as inputs. An |

MassInflowSupersonic | Mass inflow for a supersonic diffuser |

MaxShockIncidenceAngle | Compute maximum incidence angle. |

ObliqueShockAngle | Compute the oblique shock angle from the streamline deflection angle. |

PlotGasTurbineData | Generate plots from the Gas Turbine analysis functions. |

PressureRatioFromTemp | Computes pressure ratio from temperature ratio, efficiency and gamma. |

PressureTotal | Total pressure. |

PropellerEfficiency | Computes propeller efficency from Mach number. |

PropellerPower | Propeller power and induced velocity |

PropellerPowerVsV | Power vs. velocity for a propeller |

RFromCPAndGamma | Computes R from cP and gamma. |

RamRecovery | Ram recovery in an inlet. This computes the loss of pressure due to |

StaticPumping | Static pumping of air. |

StreamlineShockAngle | Compute streamline deflection angle from the oblique shock angle. |

TempRatioFromMachAndGamma | Computes the total temperature ratio from Mach number and gamma. |

TempRatioFromPressure | Computes temperature ratio |

TemperatureTotal | Total pressure. |

Theta0 | Computes the dimensionless total temperature. |

Throttle | Computes the value of the burner temperature given the throttle ratio |

TotalPressureAndTemperature | Computes the total pressure and temperature at a Mach number. |

TurboRamRocket | Model of a combined cycle engine with turbofan, ramjet and rocket. |

WriteEngineData | Write engine data to a table. |

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BldFlex | Creates the flex model interfaces. |

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ACWeightEstimation | Computes aircraft weight. Any parameter can be varied except type. |

ActiveAeroSurfacesDisplay | Color the active aerodynamic surfaces. |

AeroFormFactor | Aerodynamic form factor. |

AircraftEquilibrium | Computes the equilibrium thrust and wing area. |

AircraftGroupDataStructure | Build the AircraftGroupMass data structure. Enter parameter pairs. |

AircraftGroupMass | Create masses for an aircraft. |

AlphaFromQNV | Compute angle of attack. |

AngleOfAttackMaxLD | Angle of attack for maximum L/D. |

BankedTurn | Compute properties for a banked turn. |

BreguetRangeEquation | Computes the Breguet range. |

ClimbAngle | Compute climb angle |

ComputeAlphaConstantFlightPathAngle | Computes the angle of attack for a constant flight path angle. |

ConcordeProperties | Returns Concorde properties. |

ConstantDynamicPressureVelocity | Computes the velocity and Mach profile for constant dynamic pressure. |

DragUndercarriage | Computes drag coefficient increment due to the undercarriage. |

EnergyHeight | Compute energy height contours. |

FlightEquilibrium | Compute flight equilibrium. |

FuelFromRange | Computes the fuel as a function of range. |

Glide | Compute glide angle, range and velocity.. |

LandingDistance | Computes landing distance. |

MassCrewAndPassenger | Mass of crew and passengers. |

RateOfClimb | Computes the rate of climb and acceleration. |

SonicBoom | Compute the sonic boom scale factor. |

StallVelocity | Computes takeoff velocity. |

Takeoff | Computes the required roll distance and liftoff velocity. |

TakeoffDistance | Computes takeoff distance. |

TakeoffTransition | Compute the radius and length of transition. |

TakeoffVelocity | Computes takeoff velocity. |

TaxiingFuel | Compute taxiing fuel. |

TurningRadius | Compute turning radius and turning rate. |

VStall | Computes the stall velocity. |

WingAreaToTaper | Generates the taper and trailing edge angle for a wing. |

WingFromParameters | Generates vertices and faces for a wing based on the wing parameters. |

WingSizingForPullUp | Sizes a wing for dynamic pull up. |

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APMLinMod | Compute a linear model for a point mass aircraft at a flight condition. |

AircraftPointMassCLPSim | Simulate the controlled trajectory of a point mass aircraft model. |

AircraftPointMassControl | Compute the control inputs for a point mass aircraft model. |

AircraftPointMassDLM | Generate a discrete time-varying linear model of a point-mass aircraft. |

AircraftPointMassRHS | Compute the state derivatives of a point mass aircraft model. |

AircraftPointMassRHSWithSideslip | Point mass dynamic model with sideslip as an input. |

AircraftPointMassSim | Simulate the trajectory x(t) of a point mass aircraft model given u(t) |

RHS2DPointMass | Simulate a point mass aircraft model in 2 dimensions. |

RHS3DPointAircraft | 3D point aircraft model with time varying mass. |

SimpleLiftAndDrag | Lift and drag for the drag polar. |

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AeroCoefficientPointMass | Aerodynamic model with sideforce from a rudder. |

AeroForceAndTorqueCombined | Compute force and torque an aircraft from M = 0 to M = inf. |

CD0Composite | Drag coefficient for subsonic, supersonic and hypersonic flight. |

CDCLComposite | Lift and drag coefficients for subsonic, supersonic and hypersonic flight. |

CDCLHypersonic | Hypersonic lift and drag coefficients for a flat plate. |

CDCLSubsonic | Subsonic lift and drag coefficients for a flat plate. |

CDSkinFriction | Skin friction coefficient using a variety of models. |

CDWave | Wave drag using Ackeret theory. |

CLCMWing | Lift and moment coefficients of a thin wing. |

CLComposite | Lift coefficient for subsonic, supersonic and hypersonic flight. |

CPHypersonic | Hypersonic coefficient of pressure. |

ConcordeLD | Optimal lift and drag coefficients for the Concorde. |

DragCoeff | Computes drag coefficients for a vehicle using simple formulas. |

DragLoss | Compute drag loss using LiftAndDragJonesSearsHaack. |

DragPolar | Computes the drag polar, cD = cD0 + k*cL^2 |

DragPolarFromData | Compute the drag polar from data lift and drag coefficient data. |

FormDragCoeff | Computes form drag including wave drag. |

GroundEffect | Ground effect factor that multiplies the induced drag. |

InducedDragCoeff | Induced drag coefficient for all Mach numbers. |

LDDeltaWing | Computes the lift and drag coefficients for a swept wing |

LiftAndDrag | Computes lift and drag coefficients for a vehicle using simple formulas. |

LiftAndDragJonesSearsHaack | Lift and drag using the R.T. Jones, Sears, and Haack model. |

LiftCoeff | Computes the ideal lift coefficient from 0 through supersonic. |

LiftToDragFromMach | Computes the L/D ratio from Mach number. |

LocalAngleOfAttack | Compute the local angle of attack. |

LowSpeedAeroData | Generates a file for sc_aero_newtonian.cc/.h |

ParasiticDragCoefficient | Parasitic drag coefficient for a set of aircraft components. |

PrandtlGlauertCorrection | Computes the Prandtl Glauert Compressibility correction. |

WettedArea | Aerodynamic wetted area for different structures. |

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ACPointMassControl | Point mass control of flight path angle, velocity and angle of bank. |

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CityLatLonData.mat - provides data for city latitude and longitude |

FlatPlate.obj - a Wavefront OBJ file for a flate plate |

FlatPlateAircraft.mat - corresponding CAD model for a flate plate |

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AerodynamicHeatFlux | Heat flux as a function of mach number. |

DynamicPressureAndHeat | Heat, velocity and temperature at a fixed dynamic pressure. |

StagnationPAndT | Stagnation conditions for a gas. |

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FormFactorSurfaceOfRevolution | Computes the form factor for a body of revolution. |

FormFactorWing | Computes the form factor for a wing. |

MachSwept | Effective Mach number with sweep. |

SurfaceAreaEllipsoid | Compute the surface area of an ellipsoid. |

SurfaceAreaEllipsoidRevolution | Compute the surface area of an ellipsoid of revolution. |

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EngineDataFromTable | Generate engine data from a table. |

EngineExample | Example engine parameters. Returns a data structure. |

EngineTable | Generate an engine table for a matrix of altitudes and mach. |

JetEngine | A simple jet engine model. |

MixedFlowTurbofan | Mixed flow turbofan engine performance. |

MixedFlowTurbofanProfile | Mixed flow turbofan engine performance profile for p, h and v. |

Ramjet | Ramjet model including aerodynamic losses. The default fuel is H2. |

RamjetKerrebrock | Ramjet jet engine model producing thrust and specific fuel consumption. |

Scimitar | Models a Scimitar engine from Reaction Engines, Ltd. |

TurboRamjet | Models a turboramjet. |

Turbofan | Turbofan jet engine model produces thrust and specific fuel consumption. |

Turbofanramjet | Models a turbofanramjet. |

Turbojet | Turbojet jet engine model producing thrust and specific fuel consumption. |

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A10 | Provides two A10 aircraft models: conventional and tilt-wing. |

AIRC | AIRC aircraft model. |

CCV | CCV aircraft model. |

CCVSobel | CCV aircraft model with a pitch pointing mode. |

CreateMVSSetupFileEntries | Creates setup file entries for MultiVehicleSim |

F18Model | Generates a state space F-18 model from a range of models. |

OH6A | OH6A hover model. |

STOVL | Short Takeoff Vertical Landing aircraft model. |

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AirMass | Computes the relative air mass to sea level and a vertical path. |

AtmosphereLayers | Names the atmospheric layer for altitude h. |

GeoMagLatLon | Geomagnetic latitude and longitude. |

GeomagneticRigidity | Geomagnetic rigidity using a dipole model. |

SonicBoomHypersonic | Hypersonic sonic boom based on drag. |

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AirlinerDesign | Hypersonic airliner design. |

GroupMassStatement | Design an aircraft. |

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F100Demo | Look at the F100 model |

JetEngineAnalysisDemo | Demo JetEngineAnalysis |

JetEnginePerformanceDemo | Demo JetEnginePerformance |

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BuildFlatPlateAircraft | Create a flat plate vehicle with two flaps |

FuelConsumption | Approximate daily fuel consumption for a notional hypersonic airliner |

RamjetConstantQ | Compute ramjet thrust for a constant dynamic pressure trajectory |

StagnationTempDemo | Compute / plot the stagnation temperature vs. mach for several altitudes |

TakeoffAndLanding | Compute takeoff and landing distances for a notional hypersonic airliner |

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AircraftTrajectoryControlSim | Script to simulate aircraft trajectory control |

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ConcordeComparison | Compare Concorde with the CL and CD functions. |

NewtonianAeroDemo | Compute the L/D ratio for flat surfaces in hypersonic flow. |

SkinFrictionDemo | Skin friction and supersonic lift and drag. |

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Gust | See the response of an F16 to a gust using a state space model. |

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F135Engine | Model of the Pratt & Whitney F135 Engine. |

GenerateEngineTables | Generate ramjet and turbofan data. |

JetFlightDemo | Aircraft takeoff demo. |

RamjetDemo | Demonstrate a ramjet. |

SteadyClimb | Simulate a steady climb. |

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AIRCSim | Longitudinal simulation using the AIRC aircraft model. |

CCVEV | Demonstrate eigenvector assignment using a CCV Model |

CCVPitchPointing | Demonstrate eigenvector assignment using an STOVL Model for transition. |

L1011EV | Demonstrate eigenvector assignment using a CCV Model |

L1011EVConstraints | Demonstrate eigenvector assignment using an L1011 STOVL Model. |

LQLTR | Demonstrate linear quadratic regulator with loop transfer recovery. |

LQOF | Demonstrate linear quadratic output feedback. |

OH6ABryson | Run a linearized simulation of the OH6A. |

OH6ASim | Run a linearized simulation of the OH6A. |

STOVLEV | Demonstrate eigenvector assignment using an STOVL Model |

STOVLLatTransitionEV | Demonstrate eigenvector assignment using an STOVL Model for transition. |

STOVLLonHoverEV | Demonstrate eigenvector assignment using an STOVL Model |

STOVLLonTransitionEV | Demonstrate eigenvector assignment using an STOVL Model for transition. |

STOVLTransitionEV | Demonstrate eigenvector assignment using an STOVL Model for transition. |

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Atmosphere | Generate plots and a latex table of atm. properties across altitude. |

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NOAAWindDemo | Demonstrates NOAA Wind Model for obtaining wind data and plotting it. |

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NewtonianAeroTable | Generates a file for sc_aero_newtonian.cc/.h |

NewtonianAerodynamicsFromCAD | Compute force and torque for a CAD model. |

NewtonianAlphaFromCAD | Compute the static angle of attack to balance gravity. |

NewtonianCPFromCAD | Compute the center of pressure from the cad model. |

NewtonianForceFromCAD | Compute force and torque for a CAD model. |

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Pilot | Build a pilot model |

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CityCodeLatLonParser | Parse a string representation of U.S. city lat/lon data into a MATLAB |

HorizontalWind | Horizontal wind model HWM93 covering all altitude regions |

MergeNOAAWindData | Merge two NOAA wind data sets. There are two possibilities: |

NOAAWindData | Load wind data from the NOAA web site. The web site is: |

PlotWindField | Plot the wind field from a data structure array. |

WindFunction | Approximate the Horizontal Wind Model (HWM93) with analytic functions |

WindGust | Wind gust model. Generates state space equations or spectral densities. |

WindModel | Combined steady-state and gust model for wind. To be used in simulation. |

WindTrendsDemo | Animate the variation of wind magnitude and direction. |

WindsGUI | GUI for generating wind data over a range of parameters |

WindsPlot | Generate 3D plots of wind data vs. altitude, latitude, longitude, time. |

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SVN Revision: 42425

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