For a member with a constant cross section the following expression applies:
The expression for Stiffness can easily be derived as:
For a member with a constant cross section the following expression applies:
The expression for Stiffness can easily be derived as:
For a member with a constant cross section the following expression applies:
The expression for Stiffness can easily be derived as:
The Abbott Aerospace Technical Library is made possible by generous donations from our users. Please help us to maintain, improve and expand the library by making a contribution, giving us the means to expand our free technical library to include even more useful tools and references.
To make a one-time donation, select the PayPal button below. A donation of any amount is greatly appreciated.