Open isso11 opened 4 years ago
I can tell my e-mail address. but if you have some issues, you would asked here.
Thank you for replying. I'm setting up a simulation model for a glider in Simulink. I started with estimating the aerodynamic coefficients of the glider via MissileDatcom. I want to know the block structure of the aerodynamic model inside Simulink. I mean, for example, the Lift force coefficient is:
How can I estimate CL_de ? Which lift coefficients in the file 'for006.dat' that correspond with the coefficients in the above equation?
I have constructed this block model for the longitudinal aerodynamics. Is this construction right?
I hope I have clarified what I need help for, since it's a bit difficult to explain stuff here.
Thanks in advance
Hi Ina, I would appreciate if you can help me with some issues concerning rocket aerodynamics. I would like to contact with you. Would you please type your e-mail address ? many thanks