| Modelica.SIunits.Length | rMean | | mean radius of blade |
| Modelica.SIunits.Length | rTip_1 | | tip radius, LE |
| Modelica.SIunits.Length | rHub_1 | | hub radius, LE |
| Modelica.SIunits.Length | rTip_2 | | tip radius, TE |
| Modelica.SIunits.Length | rHub_2 | | hub radius, TE |
| Modelica.SIunits.Length | diamDisk_1 | | |
| Modelica.SIunits.Length | diamDisk_2 | | |
| Modelica.SIunits.Length | diamEffTip_1 | | |
| Modelica.SIunits.Length | rEffTip_1 | | |
| Modelica.SIunits.Length | lAxial | | axial length of blade |
| Modelica.SIunits.Length | height_1 | | blade height, LE |
| Modelica.SIunits.Length | height_2 | | blade height, TE |
| Modelica.SIunits.Length | hBlade | | blade height, avg |
| Modelica.SIunits.Area | Sblade | | surface area of single blade |
| Real | AR | | aspect ratio |
| Real | BR_1 | | boss ratio, leading |
| Real | BR_2 | | boss ratio, trailing edge |
| Real | numBlade | | num. of blades |
| Modelica.SIunits.Area | AmechAx_1 | | |
| Modelica.SIunits.Area | AmechAbs_1 | | |
| Modelica.SIunits.Area | AeffAx_1 | | eff. rep. area, flow cross section, axial, LE, NOT mech area |
| Modelica.SIunits.Area | AeffAbs_1 | | eff. rep. area, flow cross section, abs, LE, NOT mech area |
| Modelica.SIunits.Velocity | c1 | | abs-V, LE |
| Modelica.SIunits.Velocity | cx1 | | axial-V, LE |
| Modelica.SIunits.Velocity | cTheta1 | | tangential component, abs-V, LE |
| Modelica.SIunits.Velocity | w1 | | rel-V, LE |
| Modelica.SIunits.Velocity | wTheta1 | | tangential component, rel-V, LE |
| Modelica.SIunits.Velocity | c2 | | abs-V, TE |
| Modelica.SIunits.Velocity | cx2 | | axial-V, TE |
| Modelica.SIunits.Velocity | cTheta2 | | tangential component, abs-V, TE |
| Modelica.SIunits.Velocity | w2 | | rel-V, TE |
| Modelica.SIunits.Velocity | wTheta2 | | tangential component, rel-V, TE |
| Modelica.SIunits.Velocity | Utip_1 | | tangential velocity, tip, LE |
| Modelica.SIunits.Velocity | Utip_2 | | tangential velocity, tip, TE |
| Modelica.SIunits.Velocity | Umean | | tangential velocity, mean r |
| Modelica.SIunits.Angle | alpha1 | | flow angle, abs, LE |
| Modelica.SIunits.Angle | beta1 | | flow angle, rel, LE |
| Modelica.SIunits.Angle | phi1 | | angle btwn rel-V and disk plane, LE |
| Modelica.SIunits.Angle | alpha2 | | flow angle, abs, TE |
| Modelica.SIunits.Angle | beta2 | | flow angle, rel, TE |
| Modelica.SIunits.Angle | phi2 | | angle btwn rel-V and disk plane, TE |
| Modelica.SIunits.Angle | inci1 | | incident angle(AoA for airfoil), LE |
| Modelica.SIunits.Angle | xi | | angle of blade chord line |
| Modelica.SIunits.Angle | epsiron2 | | downwash angle, TE |
| Modelica.SIunits.MassFlowRate | m_flow_single | | m_flow, single blade |
| Modelica.SIunits.MassFlowRate | m_flow | | m_flow, entire disk |
| Real | CL | | lift coefficient |
| Real | CD | | drag coefficient |
| Modelica.SIunits.Force | FthetaSingle | | aero-force, tangential direction, single blade |
| Modelica.SIunits.Force | FaxSingle | | aero-force, axial direction, single blade |
| Modelica.SIunits.Force | FliftSingle | | lift, single blade |
| Modelica.SIunits.Force | FdragSingle | | drag, single blade |
| Modelica.SIunits.Force | FresultantSingle | | resultant force, single blade |
| Modelica.SIunits.Force | Ftheta | | aero-force, tangential direction, total of blades |
| Modelica.SIunits.Force | Fax | | aero-force, axial direction, total of blades |
| Modelica.SIunits.Force | Flift | | lift, total of blades |
| Modelica.SIunits.Force | Fdrag | | drag, total of blades |
| Modelica.SIunits.Force | Fresultant | | resulttant force, total of blades |
| Modelica.SIunits.Torque | trqSingle | | torque, by single blade |
| Modelica.SIunits.Power | pwrSingle | | power, by single blade |
| Modelica.SIunits.Power | pwrPropulsive | | power of propulsion, =thrust*flowSpeed |
| Real | FliftqFdrag | | lift/drag of mean line blade |
| Real | FaxqFtheta | | axial-force/tangential force |
| Real | effPropeller | | propeller efficiency, =pwrPropulsive/pwr |
| Modelica.SIunits.SpecificEnthalpy | dht | | rise in specific enthalpy across rotor |
| Real | aeroLoading | | dht/U^2 |
| Real | ratioAdv | | propeller advance ratio |
| Real | cThrust | | |
| Real | cTorque | | |
| Real | cPower | | |
| Modelica.SIunits.SpecificEnthalpy | h_1 | | enthalpy, total state |
| Modelica.SIunits.SpecificEnthalpy | h_1rel | | enthalpy, total state, relative |
| Modelica.SIunits.SpecificEnthalpy | h_2 | | enthalpy, total state |
| Modelica.SIunits.SpecificEnthalpy | h_2rel | | enthalpy, total state, relative |
| Modelica.SIunits.SpecificEnthalpy | h_1stat | | enthalpy, static state |
| Modelica.SIunits.SpecificEnthalpy | h_2stat | | enthalpy, static state |
| Modelica.SIunits.Power | pwr | | power via shaft, positive if fluid generates power |
| Modelica.SIunits.Torque | trq | | trq via shaft |
| Modelica.SIunits.AngularVelocity | omega | | mechanical rotation speed, rad/sec |
| Modelica.SIunits.Angle | phi | | mechanical rotation displacement, rad |
| Modelica.SIunits.Conversions.NonSIunits.AngularVelocity_rpm | Nmech | | mechanical rotation speed, rpm |
| Boolean | flagBladeStall | | flag, prop. blade is stalled or not |
| Modelica.SIunits.SpecificEnthalpy | rothalpy1 | | |
| Modelica.SIunits.SpecificEnthalpy | rothalpy2 | | |
| Medium.BaseProperties | fluid_amb | | flow station of inlet |
| AircraftDynamics.Aerodynamics.BaseClasses.AirfoilSimple00 | airfoilSimple001 | | |
Medium