Develop Fixed Wing Drone Airfoil with Plain and Leading-Edge Flaps. Part 1 Xfoil Analysis

Development of Fixed Wing Drone Airfoil with Plain Flap and Leading Edge Droop Flap to Maximize Range, Loiter and Minimize Takeoff and Landing Speed at Reynolds number 100000 (RE 100000) STOL Short Takeoff and Landing

Part 1: Automate Xfoil 2-dimensional airfoil analysis program with batch file
to quickly analyze many plain flaps and leading-edge droop flaps

Part 2: Verification Testing, Flight Testing

Part 3: Design Iterations and Improvements

Plain Flaps and Leading Edge droop flaps to change wing from low drag configuration for cruising to optimal loiter and takeoff or landing configuration.
Drone STOL short takeoff and landing improvement
Drone Loiter improvement
Drone duration improvement
Drone range improvement
Develop small drone for long range
Develop small drone with improved loiter time
Develop small drone with high lift wing
First time Xfoil user friendly
For first time Xfoil users
Xfoil script file examples
Xfoil batch file to speed up analysis
Xfoil optimal PPAR and ASEQ values
Xfoil compare results to wind tunnel tests
Xfoil compare result to experimental or empirical data
Airfoil data files in Xfoil format
Airfoil coordinates in Xfoil format
Drone wing with low Reynolds number
Drone wing with Reynolds number 100000
Coefficient of lift
Coefficient of drag
Xfoil accuracy
Verification of Xfoil accuracy
Compare Xfoil results to wind tunnel test results
Novel design of leading edge and trailing edge flap servo or actuator