Definition at line 34 of file flight_condition.h.
#include <flight_condition.h>
◆ FlightCondition()
MAST::FlightCondition::FlightCondition |
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◆ ~FlightCondition()
virtual MAST::FlightCondition::~FlightCondition |
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◆ init()
void MAST::FlightCondition::init |
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◆ p0()
Real MAST::FlightCondition::p0 |
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◆ q0()
Real MAST::FlightCondition::q0 |
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const |
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◆ rho()
Real MAST::FlightCondition::rho |
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const |
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◆ rho_e()
Real MAST::FlightCondition::rho_e |
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const |
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◆ rho_e_sens_mach()
Real MAST::FlightCondition::rho_e_sens_mach |
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const |
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◆ rho_e_sens_rho()
Real MAST::FlightCondition::rho_e_sens_rho |
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const |
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◆ rho_sens_rho()
Real MAST::FlightCondition::rho_sens_rho |
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const |
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◆ rho_u1()
Real MAST::FlightCondition::rho_u1 |
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const |
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◆ rho_u1_sens_mach()
Real MAST::FlightCondition::rho_u1_sens_mach |
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const |
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◆ rho_u1_sens_rho()
Real MAST::FlightCondition::rho_u1_sens_rho |
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const |
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◆ rho_u2()
Real MAST::FlightCondition::rho_u2 |
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const |
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◆ rho_u2_sens_mach()
Real MAST::FlightCondition::rho_u2_sens_mach |
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◆ rho_u2_sens_rho()
Real MAST::FlightCondition::rho_u2_sens_rho |
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const |
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◆ rho_u3()
Real MAST::FlightCondition::rho_u3 |
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const |
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◆ velocity_magnitude()
Real MAST::FlightCondition::velocity_magnitude |
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const |
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Velocity magnitude, whose direction is evaluated from the Euler angles.
Definition at line 77 of file flight_condition.h.
◆ enable_shock_capturing
bool MAST::FlightCondition::enable_shock_capturing |
flag to turn on/off artificial dissipation for shock capturing terms in fluid flow analysis.
This is true
by default.
Definition at line 52 of file flight_condition.h.
◆ flow_unit_vector
◆ gas_property
◆ inf_sol
◆ mach
Real MAST::FlightCondition::mach |
◆ ref_chord
Real MAST::FlightCondition::ref_chord |
The documentation for this class was generated from the following file: