|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: ACPro/ACEngine
% Mass inflow for a supersonic diffuser -------------------------------------------------------------------------- Form: mA = MassInflowSupersonic( gamma, machNo2, piD, p0, t0, tauR ) -------------------------------------------------------------------------- ------ Inputs ------ gamma (1,1) Ratio of specific heats machNo2 (1,1) Mach number at station 2 piD (1,1) Diffuser pressure ratio (nearly 1) altitude (1,1) Altitude (m) cP (1,1) Specific heat constant pressure machNo (1,:) Mach number units (1,:) 'eng' or 'mks' ------- Outputs ------- mA (1,:) mdot/a --------------------------------------------------------------------------
ACPro: ACEngine/AOverAStar ACPro: ACEngine/MassFlowParameter Common: Atmosphere/StdAtm Common: Graphics/Plot2D
Back to the ACPro Module page