Forum
Important Notice for New User Registrations
To combat an increasing number of spam and bot registrations, we now manually approve all new user registrations. While this may cause a delay until your account is approved, this step is essential to ensure the quality and security of this forum.
To help us verify your registration as legitimate, please use a clear name as user name or an official email address (such as a work, university, or similar address). If you’re concerned that we may not recognize your registration as non-spam, feel free to email us at with a request to approve your username.
Export Current TurbineSimulation Results in ASCII
Quote from KNunoura on 27. November 2023, 05:33Could you pleas advise me the definition of each result in “Export Current TurbineSimulation Results in ASCII”, such as Normalized Curved Length Blade 1 PAN 1[-], Structural Torsion Rate Blade 2 PAN4, …?
I cannot find out the definition in your User manual.
BR,
Kensaku
Could you pleas advise me the definition of each result in “Export Current TurbineSimulation Results in ASCII”, such as Normalized Curved Length Blade 1 PAN 1[-], Structural Torsion Rate Blade 2 PAN4, …?
I cannot find out the definition in your User manual.
BR,
Kensaku
Quote from David on 27. November 2023, 13:20Hello Kensaku,
these outputs (PAN) refer to the aerodynamic panels with which the rotor is discretized. These are the same outputs as the outputs that are plotted in the “aerodynamic blade graph“, where each PAN variable represents one aerodynamic panel.
You can also find the same outputs, interpolated at an arbitrary rotor position, in the “aerodynamic time graph” when looking at the … (at section) variables.
BR,
David
Hello Kensaku,
these outputs (PAN) refer to the aerodynamic panels with which the rotor is discretized. These are the same outputs as the outputs that are plotted in the “aerodynamic blade graph“, where each PAN variable represents one aerodynamic panel.
You can also find the same outputs, interpolated at an arbitrary rotor position, in the “aerodynamic time graph” when looking at the … (at section) variables.
BR,
David