Path: ACPro/Airbreathing
-------------------------------------------------------------------------- Models a Scimitar engine from Reaction Engines, Ltd. Uses lookup tables from publicly available data. It interpolates from the input data. This model doesn't use d or q. The model assumes a particular Mach number altitude profile. Type Scimitar for a demo. Since version 2014.1 -------------------------------------------------------------------------- Form: [t, sFC, h] = Scimitar( m, d, q ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,1) Mach number d (1,1) Engine data structure (not used) q (1,1) Standard atmosphere (not used) ------- Outputs ------- t (1,1) Thrust (N) sFC (1,1) Specific Fuel Consumption (kg/N-s) h (1,1) Assumed altitude (m) -------------------------------------------------------------------------- Reference: https://spiral.imperial.ac.uk:8443/bitstream/10044 /1/1456/1/EUCASS07_scimitar_5_08_03.pdf --------------------------------------------------------------------------
Common: Graphics/Plot2D
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