Path: ACPro/Airbreathing
% Demonstrate a ramjet. Shows specific impulse and thrust ratio as a function of Mach number. Each line in the plot is for velocities from Mach 1 to Mach 4.5 and for a different altitude profile. This model includes non-ideal pressure ratios for the diffuser, nozzle and combustor. ------------------------------------------------------------------------ See also StdAtm, Plot2D, Ramjet, UE ------------------------------------------------------------------------ % -------------------------------------------------------------------------- Copyright (c) 2007 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
ACPro: Airbreathing/Ramjet AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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