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ILD as system-specific; focal point recurrence

Short answer

An influence line is system-specific: it depends only on spans, supports and stiffness, not on loading, and can be used for any load once drawn. For loading on the right, the left focal ratio recurrence is k_{n+1} = (L_{n+1}/I_{n+1})/[(2-k_n)L_n/I_n + 2L_{n+1}/I_{n+1}], with hinged end k = 0 and fixed end k = 1/2.

Explain influence line diagram as a system specific diagram. Derive the expression of the recurrent formula for focal point ratio considering two consecutive spans for loading on right spans.

ILD as a system-specific diagram

An influence line shows how one response (a reaction, shear or moment at one fixed location) varies as a unit load moves over the structure. It depends only on the system: the spans, support types, flexural rigidities and the chosen response, and not on the loads. So:

  • the ILD of RBR_B for a propped cantilever (zero at A, 1 at B, curved between) is quite different from that of a simply supported beam of the same length, and a beam with spans 6 m + 8 m has different ILDs from one with 8 m + 8 m;
  • once the ILD for a system is drawn, it can be used for any loading on that same system: Q=∑PiyiQ = \sum P_i y_i for point loads, Q=w×(area of ILD under the load)Q = w\times(\text{area of ILD under the load}) for a UDL.

By contrast, a BMD or SFD is load-specific: it shows one response along the whole beam for one given loading. An ILD is system-specific and response-specific.

Recurrence formula of the left focal ratio (loading on right spans)

Consider a continuous beam with spans numbered from the left; span nn lies between supports n−1n-1 and nn, with length LnL_n and moment of inertia InI_n. Let the load be on a span to the right of span n+1n+1 (all spans from the left end up to n+1n+1 unloaded), and let moments be taken with one sign convention (hogging or sagging) at all supports.

Three-moment equation at support nn for the unloaded spans nn and n+1n+1 (the load terms are zero):

Mn−1LnIn+2Mn(LnIn+Ln+1In+1)+Mn+1Ln+1In+1=0M_{n-1}\frac{L_n}{I_n} + 2M_n\left(\frac{L_n}{I_n}+\frac{L_{n+1}}{I_{n+1}}\right) + M_{n+1}\frac{L_{n+1}}{I_{n+1}} = 0

Because the moment in an unloaded span is linear, the moments at its two ends have opposite signs and a fixed ratio. Define the left focal ratio of span nn:

kn=−Mn−1Mnk_n = -\frac{M_{n-1}}{M_n}

and similarly for span n+1n+1: Mn=−kn+1Mn+1M_n = -k_{n+1}M_{n+1}.

Substitute Mn−1=−knMnM_{n-1} = -k_nM_n in the equation:

Mn[(2−kn)LnIn+2Ln+1In+1]=−Mn+1Ln+1In+1M_n\left[(2-k_n)\frac{L_n}{I_n} + 2\frac{L_{n+1}}{I_{n+1}}\right] = -M_{n+1}\frac{L_{n+1}}{I_{n+1}}

so that Mn/Mn+1=−kn+1M_n/M_{n+1} = -k_{n+1} gives the recurrence formula

 kn+1=Ln+1/In+1(2−kn) Ln/In+2 Ln+1/In+1 \boxed{\,k_{n+1} = \frac{L_{n+1}/I_{n+1}}{(2-k_n)\,L_n/I_n + 2\,L_{n+1}/I_{n+1}}\,}

For equal spans with constant EIEI this becomes kn+1=14−knk_{n+1} = \dfrac{1}{4-k_n}.

Starting value: if the left end of the beam is hinged, M0=0M_0 = 0 so k1=0k_1 = 0; if it is fixed, the slope there is zero, 2M0+M1=02M_0 + M_1 = 0, so k1=12k_1 = \tfrac12.

Focal point: the straight BMD of unloaded span nn is M(x)=Mn[1−(1+kn)xLn]M(x) = M_n\left[1 - (1+k_n)\dfrac{x}{L_n}\right], with xx measured from support nn, so it crosses the beam axis at x=Ln1+knx = \dfrac{L_n}{1+k_n} from support nn. This point is the left focal point, and it is the same for any loading on the spans to the right of span nn.

✓ Answer checked by Claude Opus 5.5 (high effort)

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