Stark/AMI utilizes a full suite of design and analysis methods for the sizing and assessment of new aircraft configurations and modifications to existing configurations. Our inverse design methods incorporate our low and high-order CFD methods to quickly and efficiently localize an optimum configuration.
Surface sizing techniques combined with our in-house empirical-based mission performance program are ideal for the geometric optimization of each aircraft in its particular mission. Further aerodynamic analyses are available through VLAERO+ for stability and control information, and specific flow field details can be interrogated through Navier-Stokes solutions for powerplant and fairing integration.
Our large library of analysis tools provide further design optimization for most other aircraft components and systems.