Path: ACPro/ACDesign
% Computes aircraft power and thrust for a set of trajectory segments.
The built-in demo is for a Boeing 737-800
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Form:
l = AircraftPowerAndThrust( s, d )
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Inputs
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s (1,:) Vector of trajectory segment data structures
.phase (1,:) Character array containing the name of
this segment
.v (1,1) Velocity of this segment. If v<3, assumes
v is the Mach number. (m/s or Mach)
.h (1,1) Starting altitude of this segment (m)
.rateOfClimb (1,1) Rate of climb of this segment (m/s)
.range (1,1) If rateOfClimb is zero, the range of this
segment (m). If rateOfClimb is not zero,
range is automatically computed.
d (.) Aircraft data structure, by default produced by Boeing737.m
.mass (1,1) Max takeoff mass (kg)
.sFC (1,1) Thrust-specific fuel consumption, kg/s*N
.e (1,1) Oswald efficiency
.aR (1,1) Aspect ratio
.s (1,1) Wing area (m^2)
.cD0 (1,1) Zero-lift drag coefficient, clean
.cLAlpha (1,1) Coefficient of lift over angle of attack
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Outputs
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l {} Table of results, or l = struct('s','d'}
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ACPro: ACDesign/AircraftThrustFromFlight ACPro: ACDesign/Boeing737 ACPro: ACProAerodynamics/InducedDragCoeff ACPro: ACUtils/FLToM AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/DisplayLatexTable Common: General/ListCases Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PlotDoubleYAxis Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS
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