Request to add spanwise loading and chord wise loading output based on ID

[Preethamkadambi]

As the title suggests,

1. Is there a way to export spanwise aero-loading and chord wise loading?
   I wanted to compare Schrenks method, ANC-1 and ANC-2 results with DVLM and VLM results.
   2.Is it possible to define control surfaces and their deflections?

[ArneVoss]

Hello Preetham,
both the VLM and the DLM produce a so-called AIC matrix, which can be used to calculate the pressure distribution cp based on the downwash wj per panel: cp = AIC * wj
The rest is up to you - if you are interested in a span- or chord-wise pressure distribution, I propose to integrate over the panels in the desired direction. Control surface deflections are modeled by an additional downwash on the corresponding aerodynamic panels.
Does this help you?