RAM Structural System Help

Direct Analysis Method

The Direct Analysis Method requires:
  1. 2nd order analysis (either an iterative 2nd order analysis of amplified 1st order analysis), including both P-Δ and P-δ
  2. Notional loads
  3. Reduced flexural and axial stiffness

Second Order Analysis

The amplified 1st order analysis is implemented and it involves the calculation of B1 and B2 factors by which the member forces are multiplied. The advantage to this method is that it does not require an iterative analysis and it would allow the analysis of individual load case, with the results combined in the load combinations (the principle of superposition).

Notional Loads

Notional loads are required to be applied. If the ratio of 2nd order drift to 1st order drift (i.e., B2) is greater than 1.5, the notional loads must be applied in addition to the other lateral loads (wind and seismic); if the ratio is less than 1.5, it is permissible to apply the notional loads to the gravity-only combinations.

Note: The value 1.5 is based on a model with nominal member properties. Otherwise, it is 1.7 for models with reduced member stiffness properties.
The notional loads are defined as:

Ni = 0.002 Yi

where
Yi
=
the factored gravity load(for ASD, use a factor of 1.6 on both Dead and Live load)

Reduced Stiffness

A reduced flexural stiffness is to be used for columns and beams:

EI* = 0.8 τb EI Eq. (A-7-2)

where
τb
=
1.0 when α P r P y 0.5
4 [ α P r P y ( 1 α P r P y ) ] w h e n α P r P y > 0.5
α
=
1.0 for LRFD and 1.6 for ASD
Pr
=
total axial load in the member (combined using the appropriate LRFD or ASD Load Combinations)
Py
=
AsFy
Note: In the second case the analysis must be iterative since Pr is a function of τb and vice versa. In lieu of that, the Specification permits the application of an additional notional load equal to 0.001 Yi
A reduced axial stiffness is also to be used:

EA* = 0.8 EA Eq. (A-7-3)