Path: ACPro/ACEngine
% Engine performance map from a table lookup.
Rows are altitude, columns Mach number. It will plot 2D meshes.
If h or m are outside the range of d.h or d.m, it will give an error.
Type EngineMap for a demo using JetEngine as the source.
--------------------------------------------------------------------------
Form:
[iSp, fS] = EngineMap(h,m,d)
d = EngineMap;
--------------------------------------------------------------------------
------
Inputs
------
h (1,:) Altitude (m)
m (1,:) Mach number
d (.) Data structure
.h (1,:)Altitude (m)
.m (1,:) Mach number
.iSp (:,:) Specific impulse (s)
.fS (:,:) Specific thrust (N/kg/s)
-------
Outputs
-------
iSp (:,:) Specific impulse (s)
fS (:,:) Specific thrust (N/kg/s)
--------------------------------------------------------------------------
See also: JetEngine.
--------------------------------------------------------------------------
ACPro: Airbreathing/JetEngine AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect
Back to the ACPro Module page