[varghese9]

does the same apply for typical wing section module .as stated in jj alonso paper the wing is first kept in pitching for 3 cyles then the free response is measured for 2d flutter solution removing the holding pin .can i use the pitching case first as direct analysi for time equal t= 0.33 sec and later setup the 2d config file for flutter using the class solver typical wing section and use the last 2 output from pitching case to start the flutter response by switching to restart option with changing the file name of pitching case to solution _flow .dat from restart_flow .dat and run the response if not what should be the correct procedure.let me know if possible ----