Calculation of forces and moments acting on the wing
Employer
[no-member:pro]Roman[/no-member:pro]
Project parameters
Type of cooperationOne-time project
SectionEngineering. Drawings
Prepaymentwithout prepayment
Payment methodsBank transfer
Acceptance of requestsfrom Apr 18, 2025 until Apr 28, 2025
Project description
Offering earnings for a specialist in calculations in Open Foam. Using the Open Foam computational package, you need to calculate the forces and moments acting on the wing. The wing is moving at a slip angle.
It's vertical. The slope is carried out along a line rotated 30 degrees to the vector of the incoming flow. The angle of the installation (attack) of the wing is shown in the figure.
The angle of inclination in the vertical plane varies from -10 to +20 degrees.
We must find the longitudinal and transverse components of the force and moment, relative to the vertical axis passing through the lower point of rotation of the wing.
In the calculation, consider two options: a flat plate and an arc, curved in the shape of the NACA0010 profile.
It's vertical. The slope is carried out along a line rotated 30 degrees to the vector of the incoming flow. The angle of the installation (attack) of the wing is shown in the figure.
The angle of inclination in the vertical plane varies from -10 to +20 degrees.
We must find the longitudinal and transverse components of the force and moment, relative to the vertical axis passing through the lower point of rotation of the wing.
In the calculation, consider two options: a flat plate and an arc, curved in the shape of the NACA0010 profile.
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