Hi man,
that is a so called "singular integral". See http://en.wikipedia.org/wiki/Singular_integral.
There are specific numerical methods for solving this kind of problem.
Hi dudes!
I need to study a rotating flapping wing subjected to angular velocity depending on time with Nastran.
I found that Nastran does not calculate correctly the centrifugal forces and deformations in the case of the SOL Transient Dynamic/Time History,
while the forces and deformations...
Hi dudes!
I need to study a rotating flapping wing subjected to angular velocity depending on time with Nastran.
I found that Nastran does not calculate correctly the centrifugal forces and deformations in the case of the SOL Transient Dynamic/Time History,
while the forces and deformations...
Hi dudes!
I need to study a rotating flapping wing subjected to angular velocity depending on time with Nastran.
I found that Nastran does not calculate correctly the centrifugal forces and deformations in the case of the SOL Transient Dynamic/Time History,
while the forces and deformations...
Hi, thank you for replying.
I tried to give separate load cases for each direction but I can do that only a static analisis,
The SOLUTION 601, which is the Advanced Nonlinear Transient, can analyze only one bodyload per time.
Anyother tip? appreciate it!
Hi dudes,
I'm studying micro flapping vehicles.
I need to evaluate the inertial forces due to the angular velocity of the wing during a cycle.
The angular velocity varies in strength and in direction
I found the way for setting on NX Nastran an angular velocity with varying strength but I did...
