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PSS Thermal Module
MATLAB toolboxes for aerospace analysis
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PSS Thermal Module
MATLAB toolboxes for aerospace analysis
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| ▼ Aerospace | |
| ▼ Thermal | |
| ▼ Brayton | Brayton cycle and engine designs |
| BraytonIdeal.m | Ideal Brayton cycle |
| BraytonWithRecuperator.m | Brayton Cycle with Recuperator |
| ▼ Demos | Thermal demos |
| ▼ ThermalAnalysis | |
| SCThermalDemo.m | Demonstrates how to use the thermal modeling package Published Demo |
| SimpleBraytonCycle.m | Analysis of an ideal Brayton cycle Published Demo Assumes the compressor and turbine are 100% efficient |
| ThermalEquilibriumBox.m | Thermal equilibrium examples |
| ThreeNodeNetwork.m | Demonstrate Thermnet with a three node model |
| TNet.m | Demonstrate Thermnet |
| ▼ ThermalControl | |
| LQThermalControl.m | Design a linear quadratic temperature controller Published Demo |
| ▼ ThermalGraphics | |
| ThermalCube.m | Create a simple satellite with 6 panels for thermal analysis |
| ▼ HeatExchanger | |
| AbsoluteViscosity.m | 10e-5 Pa-s |
| FrictionLaminar.m | Demo |
| HeatExchanger.m | Designs a heat exchanger for a one sided heat flux |
| HeatExchangerWithLosses.m | Demo |
| HeatTransferChannel.m | Designs a heat exchanger for a one sided heat flux |
| HeatTransferCoeff.m | Computes the Heat transfer coefficient |
| KinematicViscosity.m | Computes the Kinematic viscosity |
| NusseltDeveloping.m | Computes the Nusselt number for developing turbulent flow |
| NusseltLaminar.m | Computes the Nusselt number for laminar flow |
| NusseltTurbulent.m | Computes the Nusselt number for fully developed turbulent flow |
| PrandtlNikuradse.m | Computes the Fanning friction factor for fully developed turbulent flow |
| PrandtlNumber.m | Computes the Prandtl number |
| PressureDropChannel.m | Computes the channel pressure drop |
| ReynoldsNumberKinematic.m | Computes the Reynolds number |
| ThermalConductivity.m | Computes the thermal conductivity |
| Help | |
| ▼ ThermalAnalysis | |
| AeroHeatFlux.m | Demo |
| BTUToJoule.m | Converts BTUs to Joules |
| FSolarPanelThermal.m | Used by fmins from SolarPanelThermal to compute panel temperatures |
| GrayBody.m | Aborptivity and emissivity of a gray body |
| Isothermal.m | Add the incoming radiation (qIn) and power and subtract the outgoing radiation (qOut) |
| IsothermalHelio.m | Isothermal model in heliocentric orbit |
| IsothermalLunar.m | Model a spacecraft as an isothermal radiator in lunar orbit |
| JouleToBTU.m | Converts Joules to BTUs |
| LambertL.m | Demo |
| OptimalMLIDensity.m | Determine optimal Multi-layer Insulation (MLI) density |
| PanelThermalModel.m | Computes the temperatures of a panel from a CAD model |
| PlanckL.m | Demo |
| RadBFp.m | Radiation between equal area flat plates |
| RadDa.m | Radiation from an incremental area |
| RadiationShapeFactor.m | Demo or default data structure |
| RHSAerodynamicHeating.m | Compute aerodynamic heating |
| RHSIsothermal.m | Model a spacecraft as an isothermal radiator |
| SolarPanelThermal.m | Compute the front/back temperatures of a solar panel |
| SpaceCamera.m | Draw spacecraft in orbit about a planet, as seen by an in-situ camera |
| SpacecraftThermal.m | The individual face vectors |
| ThermalColorMap.m | Generates a color corresponding to a temperature |
| ThermalEquilibrium.m | Built-in Demo |
| Thermnet.m | Size the system matrices |
| ▼ ThermalGraphics | |
| DrawThermalPlugIn.m | Draw a thermal diagram |
| PlotThermal.m | Plots flux and temperature |
| ThermalImager.m | Plot planet in m |
| ▼ ThermalProperties | |
| AbsDa.m | Demo |
| BlckBody.m | Aborptivity and emissivity of a black body |
| EmittanceParallelPlates.m | Demo |
| HeatFP.m | Now do a Newton Raphson |
| HeatShieldCoating.m | Values for heat shield coatings |
| RadiatorCoating.m | Values for radiator coatings |
| TempConv.m | Convert inputs to Kelvin |
| TempCyl.m | Temperature of a cylinder |
| TempFP.m | Temperature of a flat plate |
| TempSph.m | Demo |
| WiensDsp.m | Computes the peak black body wavelength as a function of temperature |
1.9.2