Am obținut, din partea Aerospace Project Development Group – ALR din Elveția, acordarea licenței gratuite pentru Aircraft Performances Program software.
APP provides you with a multitude of flight segments that allow you to define specific mission analyses. It enables both, a very fast and easy “first shot” solution up to very detailed missions for complex analyses! A selection of available segments includes: Available Flight segments
- Acceleration
- Climb; Climb at Best Angle; Climb at Best Rate; Climb at CAS; Climb at EAS; Climb at Constant Mach
- Cruise; Cruise at Best SR; Cruise at Mach; Cruise at Optimum Altitude and Mach
- Deceleration
- Descent, Descent at No Credit (at best FF or best SR), Descent at CAS, Descent at EAS, Descent at Mach
- Energy Exchange
- Ground Operation
- Landing Roll
- Loiter & Loiter at Best FF
- Maneuver at Constant or Maximum Load Factor
- Refuel
- Reset Altitude or Reset Mach
- Store Drop
- Take-off
The mission module includes a set of fast optimizers to help you refine your analyses. Using the mission-optimizers, APP users are able to define segments that shall be maximized along with inputs on required reserves. Available optimizations are:
- Range Optimization
- Endurance Optimization
- Radius of Action optimization
APP features a multitude of standard performance charts for aircraft point performance analysis. Furthermore a comparison feature for different results is readily available. Available Pre-defined point performance-analysis charts are highly customizable, they include:
- SEP-Envelopes
- G-Envelopes
- Turn-Rate Charts (constant SEP) / Energy-Maneuverability Charts
- Turn-Rate Charts (constant Altitude)
- SEP vs. Altitude Charts
- Point Performance Parameter Computation
- Required Thrust and Drag Chart for Different Load-Factors
APP incorporates a unique 2.5-dimensional method to obtain takeoff- and landing- distances with respect to different certifications and environmental conditions:
- Takeoff, Rejected Takeoff, Balanced Field Length, Landing
- Calculations respect military and civil airworthiness regulations: MIL-STD-3013, FAR Part 23 & 25, EASA CS 23 & 25
- All Engines Operative (AEO) and One Engine Inoperative (OEI) calculations
- Respecting runway dimensions as: Runway Length, Runway Altitude, Runway Slope
- Different runway conditions are available: Dry, Wet, Snow, Ice
- Calculations possible with or without afterburner
Le mulțumim pentru suportul acordat,
