Eachine Wizard X220 CAD Model Design
Budget / Salary£10–30
TypeFreelance project
LocationRemote
Posted2 hours ago
Project: Eachine Wizard X220 OpenVSP / CAD Model
I need a simplified but dimensionally representative Eachine Wizard X220 quadcopter model for OpenVSP / VSPAERO aerodynamic analysis as part of an MSc dissertation.
The model should include:
- Main body/frame
- Four arms
- Four motors
- Propellers or simplified rotor discs
- Battery/electronics volume where aerodynamically relevant
The main reference dimension is approximately 220 mm diagonal motor-to-motor wheelbase.
The priority is accurate:
- Overall dimensions
- Motor positions
- Arm geometry
- Central body geometry
- Propeller diameter
- Frontal/projected area
Small details such as screws, wires and antennas are not required.
OpenVSP Requirements
Preferred output is native OpenVSP geometry suitable for:
- VSPAERO
- Rotor-off / bare-airframe analysis
- Rotor-on modelling
- Different wind speeds
- Different angles of attack
Deliverables
- .vsp3 OpenVSP file
- STEP/CAD file if available
- STL export
- Main dimensions used
- Brief list of modelling assumptions/simplifications
The model will be compared with wind-tunnel measurements of:
Lift, Drag, Side Force, Pitching Moment, Rolling Moment and Yawing Moment.
Manufacturing-level detail is not required. The main aim is a reliable aerodynamic model of the Wizard X220 for OpenVSP/VSPAERO analysis.
I need a simplified but dimensionally representative Eachine Wizard X220 quadcopter model for OpenVSP / VSPAERO aerodynamic analysis as part of an MSc dissertation.
The model should include:
- Main body/frame
- Four arms
- Four motors
- Propellers or simplified rotor discs
- Battery/electronics volume where aerodynamically relevant
The main reference dimension is approximately 220 mm diagonal motor-to-motor wheelbase.
The priority is accurate:
- Overall dimensions
- Motor positions
- Arm geometry
- Central body geometry
- Propeller diameter
- Frontal/projected area
Small details such as screws, wires and antennas are not required.
OpenVSP Requirements
Preferred output is native OpenVSP geometry suitable for:
- VSPAERO
- Rotor-off / bare-airframe analysis
- Rotor-on modelling
- Different wind speeds
- Different angles of attack
Deliverables
- .vsp3 OpenVSP file
- STEP/CAD file if available
- STL export
- Main dimensions used
- Brief list of modelling assumptions/simplifications
The model will be compared with wind-tunnel measurements of:
Lift, Drag, Side Force, Pitching Moment, Rolling Moment and Yawing Moment.
Manufacturing-level detail is not required. The main aim is a reliable aerodynamic model of the Wizard X220 for OpenVSP/VSPAERO analysis.
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