calculate_responses0¶

Source: userfiles/SSBJ/subsystem0/calculate_responses0.py

Response calculation module for SSBJ Subsystem 0 (Aircraft).

This module provides the range calculation for the aircraft subsystem of the Supersonic Business Jet (SSBJ) problem.

Functions¶

calculate_range(specific_fuel_consumption: float, lift_to_drag_ratio: float, total_weight: float, fuel_weight: float, h: float, Mach: float) → float

Calculate the aircraft range using the Breguet range equation.

Args:

specific_fuel_consumption: Specific fuel consumption coefficient [1/hr].
lift_to_drag_ratio: Lift-to-drag ratio [-].
total_weight: Total aircraft weight [lb].
fuel_weight: Fuel weight [lb].
h: Altitude in feet [ft].
Mach: Mach number [-].

Returns:

Range in nautical miles [nmi].