Features:

Aerodynamic surface based on subdividing the surfaces with force integration, similar to the blade element method (BET) for rotors.
Thermodynamic models for the Piston, Turboprop, Turbojet and Turbofan engines.
Simple table-based thrust and power engines are also available for rapid prototyping.
Spring-Mass-Damper-based wheel system, which can be extended for improved friction physics.
Streamlined setup with swappable components.
Basic and advanced flight control systems available, such as CAS, SAS and Autopilot systems
Airfoils can be configured from wind tunnel data or approximations from Xfoil & Javafoil
Instrumentation system with various levels and dials available
Section-based drag modelling for the fuselage and external surfaces
Exposed C++ functions/variables for blueprints integration and function extension

Code Modules:

Number of C++ Classes: 16

Network Replicated: (No)

Supported Development Platforms: Win64, Linux, MacOS

Supported Target Build Platforms: Win64, Linux, MacOS, Android

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