1. i want to integrate a variable (e.g pressure on the exit plane of turbine blades) varying along 'x' axis or 'radius'. (i.e at each 'x' or 'radius' it integrates over 'y' or 'theta' and then moves to next 'x' or 'radius' . How will it be possible?. i have done the CFD simulation in fluent.
2. in 'integration' dialog box > 'Over' what does i,j and k lines represent for 3D case.
3. kindly also tell how to attach an image