Calculation of forces and moments acting on a wing in OpenFOAM.

puck1 · February 21, 2023, 15:31

I need to perform calculations of the forces and moments acting on a wing using the computational package OpenFOAM. The wing moves with a sideslip angle and is vertically oriented. The inclination is carried out along a line rotated 30 degrees to the vector of the oncoming flow. The angle of attack of the wing is given in the figure. The inclination angle in the vertical plane varies from -10 to +20 degrees. It is necessary to find the longitudinal and transverse components of force and moment, relative to the vertical axis passing through the lower point of rotation of the wing. Two variants should be considered in the calculation: a flat plate and a curved wing, bent according to the NACA0010 profile.

Could you help me with her solution? I will be very grateful for your help.

puck1 · May 11, 2024, 07:54

[QUOTE=puck1;844952]It is necessary to find the longitudinal and transverse components of force and moment, relative to the vertical axis passing through the lower point of rotation of the wing.
Could you help me with her solution? I will be very grateful for your help.

February 21, 2023, 15:31	Calculation of forces and moments acting on a wing in OpenFOAM.	#1
puck1 New Member Join Date: Feb 2023 Posts: 2 Rep Power: 0	I need to perform calculations of the forces and moments acting on a wing using the computational package OpenFOAM. The wing moves with a sideslip angle and is vertically oriented. The inclination is carried out along a line rotated 30 degrees to the vector of the oncoming flow. The angle of attack of the wing is given in the figure. The inclination angle in the vertical plane varies from -10 to +20 degrees. It is necessary to find the longitudinal and transverse components of force and moment, relative to the vertical axis passing through the lower point of rotation of the wing. Two variants should be considered in the calculation: a flat plate and a curved wing, bent according to the NACA0010 profile. Could you help me with her solution? I will be very grateful for your help.

May 11, 2024, 07:54	relative to the vertical axis passing through the lower point of rotation of the win	#2
puck1 New Member Join Date: Feb 2023 Posts: 2 Rep Power: 0	[QUOTE=puck1;844952]It is necessary to find the longitudinal and transverse components of force and moment, relative to the vertical axis passing through the lower point of rotation of the wing. Could you help me with her solution? I will be very grateful for your help.

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