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Path: ACPro/Demos/ACPerformance
% Compute ramjet thrust for a constant dynamic pressure trajectory Constant dynamic pressure is often recommended for scramjet trajectories. This function computes the thrust for a ramjet. The velocity used produces constant dynamic pressure. -------------------------------------------------------------------------- Copyright (c) 2016 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2016.1 --------------------------------------------------------------------------
ACPro: ACPerformance/ConstantDynamicPressureVelocity ACPro: Airbreathing/RamjetKerrebrock Common: Atmosphere/StdAtm
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