steps
engineer the fully customized aircraft
Loads Analysis.
Calculations of V-n Diagrams, flight loads (maneuver, discrete gust, continuous gust, ground loads (landing, braking, taxing, jacking, and towing) and engine loads (engine torque and gyroscopic loads)
Trim Calculations (Rigid aircraft or flexible aircraft trim analysis)
Perform trim analysis for any state of flight to determine aircraft angle of attack, control surface deflections, load distribution, and calculate aerodynamic efficiency
Performance Calculations.
Reliable estimations for critical characteristics such as endurance, maximum steady level flight, rate of climb, determination of power requirements, etc
Static and Dynamic Stability
Determination of the aircraft?s stability margins using classical flight dynamics and/or advanced computer simulation.
Structural Design, Analysis and Optimization
Design and analysis of structures is performed using advanced composite and metallic structures. Advanced tools, such as finite element analysis, are used to aid in design, analysis and optimization of structural components. Analytical models can be validated using any available test data. Analysis is performed to determine margin of safety for each component. In addition, Optimum Solutions can perform the following tasks: