Arbitrary Surface Motion:

The Wagner Function

Assume that the response to an arbitrary airfoil motion in the linear regime can be built up as a superposition of responses to a series of step changes in normal wash.
Response of a linear system: Indicial Admittance

Apply a unit step force 1(t) to the mass m inthe +ve x direction:

The system was initially in rest at unloaded equilibrium:

.

The motion is described by 

General solution:  where 

Applying the initial conditions, we get:  .

Thus the response of the linear system to a unit step function is:

. This is called "indicial admittance". The particular functional form of A depends on the linear system being considered. The response to an arbitrary force f(t) can be built up from this.
 
 

Response at time to a step load Df applied at time t+Dt is:

Summing up,

As 

This is the Duhamel integral, in terms of the indicial admittance and the derivatives of the forcing function. The forcing function may not be available in analytic form, so we need an alternate form:

Integrate by parts, using:

where  , so that 

, so that 

Note that:

Substituting,

Thus if the indicial admittance function is known, the system response can be determined from this.
 
 

Indicial Admittance for an airfoil in pitch+plunge: Wagner Function

Unsteady lift associated with the Theodorsen function acs at the quarter chord, and is due to the normal wash at 3/4 chord. Take the normalwash as a step function:
. Take the Fourier transform of w:

. Circulatory lift coefficient is:  (taking the inverse Fourier transform). Define  as the number of semichords traveled in time t. Then
 

. This can be writen as  where f(s) is the Wagner function.

Also,  .

Note: The Wagner function is the indicial admittance for the normalized circulatory lift associated with a step change in normalwash at the 3/4-chord.

This is approximated by the following expressions:

.
These expressions are compared in the linked table and figure.