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Red Leader (talk | contribs) (Finish cleanup, almost ready for publishing. Need to wait for Screenshot of the Month contest result. PLEASE DON'T ADD ANYTHING) |
Red Leader (talk | contribs) (→AeromatiC++ 3.0 released: Missed a bit. @Erik, feel free to change the CMadot, CYbeta, etc. subscripting if they are not correct) |
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* Catapult system | * Catapult system | ||
Version 3.1.0 adds code that estimates | Version 3.1.0 adds code that estimates CL<sub>de</sub>, CM<sub>a</sub>, CM<sub>adot</sub>, CM<sub>q</sub>, CM<sub>de</sub>, CY<sub>beta</sub>, Cn<sub>beta</sub>, Cn<sub>r</sub>, Cn<sub>dr</sub>, Cl<sub>beta</sub>, Cl<sub>r</sub> and Cl<sub>p</sub> based on wing geometry. There is also support for the calculation of CY<sub>p</sub>, CY<sub>r</sub>, CY<sub>dr</sub> and Cn<sub>p</sub> based on wing geometry which previous versions did not specify. After a request from Necolatis, the turbine engine tables are now adjusted for bypass ratio. | ||
For this to work properly, you have to provide factual data. Do not try to estimate it yourself. If some data is unknown, leave it blank and AeromatiC++ will make it's own estimation or reverts to the table lookup method. | For this to work properly, you have to provide factual data. Do not try to estimate it yourself. If some data is unknown, leave it blank and AeromatiC++ will make it's own estimation or reverts to the table lookup method. |