This page documents the kinematics and dynamics analysis carried out on the PPP-106 sprint engine during its development programme. The aim was to quantify the forces acting on the piston and connecting rod assembly at maximum RPM, and to assess the stress on both OEM and uprated components. The results directly informed decisions around conrod specification and piston choice.

All values shown use the actual measured geometry of the 106 Rallye TU3 bottom end. Calculations follow the standard slider-crank model, retaining the first two terms of the Fourier series expansion - valid where R/L < 0.3.

Bore
76 mm
Stroke
77 mm
Crank Radius (R)
38.5 mm
Con-rod Length (L)
133.5 mm
R/L Ratio
0.288
Max Design RPM
8,500 rpm
R/L = 0.288 — below the 0.3 threshold. The first two Fourier terms give sufficient accuracy without needing the full series expansion.

1. Reciprocating Masses

The reciprocating mass is the total mass that the engine must accelerate and decelerate on every stroke. It comprises the piston assembly and the small-end (gudgeon pin end) fraction of the connecting rod. Reducing this mass directly reduces peak bearing loads and allows higher RPM for a given stress limit.

Component OEM (g) OEM (kg) EBD Modified (g) EBD Modified (kg)
Piston assembly 395 0.395 315 (Wossner) 0.315
Con-rod small end mass 135.5 0.1355 135.5 0.1355
Total reciprocating mass 530.5 0.5305 450.5 0.4505

The Wossner forged piston saves 80 g per cylinder compared to the OEM cast item - a 15% reduction in reciprocating mass. At 8,500 rpm this has a significant effect on peak piston force and therefore on con-rod stress.

Con-rod small-end mass was measured as 135.5 g on the EBD-modified rods. The standard rod cross-sectional area was measured at 1.0754 × 10² mm² (1.0754 × 10⁻&sup4; m²).

2. Piston Acceleration

Piston acceleration varies continuously around the cycle. Using the two-term approximation, instantaneous acceleration a at crank angle θ is:

a = R ω² (cosθ + (R/L) cos 2θ)
R = crank radius (m) ω = angular velocity (rad/s) = 2πN/60 θ = crank angle (0° at TDC) L = con-rod length (m)

At θ = 0° (TDC) both cosine terms are +1, giving maximum positive acceleration — the piston is being pulled to a halt and reversed. This is where peak tensile load is applied to the con-rod small end.

Angular Velocity (ω)
890.1 rad/s
at 8,500 rpm
Peak Piston Acceleration
39,301 m/s²
at TDC (θ = 0°)
Avg Piston Speed
21.8 m/s
= 2 × stroke × N/60
Max Piston Speed
35.6 m/s
peak instantaneous

3. Peak Piston Force

The peak inertia force on the con-rod is found from F = m × a, using the total reciprocating mass and the peak acceleration calculated above. This force acts in tension at TDC on the overrun (or on a non-firing stroke).

F = M × amax
M = total reciprocating mass (kg) amax = peak piston acceleration (m/s²) F = peak inertia force (N)
Configuration Reciprocating Mass Peak Acceleration Peak Force
OEM components 530.5 g (0.5305 kg) 39,301 m/s² 20,849 N
EBD modified (Wossner piston) 450.5 g (0.4505 kg) 39,301 m/s² 17,705 N (3,144 N saving)

4. Con-Rod Stress Analysis

With the peak force known, the nominal tensile stress in the con-rod shank is calculated from the measured cross-sectional area. This gives a conservative estimate — the actual stress distribution is non-uniform, but this gives a useful baseline for material selection and factor-of-safety assessment.

σ = F / A
σ = nominal stress (MPa) F = peak inertia force (N) A = con-rod CSA = 107.54 mm²
Configuration Peak Force Con-rod CSA Nominal Stress Rod UTS (material) Factor of Safety
OEM piston 20,849 N 107.54 mm² 193.9 MPa 430 MPa 2.22
EBD modified (Wossner) 17,705 N 107.54 mm² 164.6 MPa 430 MPa 2.61
Rod material tensile strength assumed at 430 MPa — representative of a normalised medium-carbon steel (e.g. EN8 / 080M40). Factors of safety above 2.0 are considered acceptable for a motorsport engine at this stress level. Note that this analysis considers inertia loading only — gas pressure loads during combustion are additive on the compression stroke and must be assessed separately for a full picture.

Well-designed connecting rods do not fail under the compressive inertia load alone — the Euler buckling load for the rod geometry is significantly higher than the peak compressive force. Failure, when it occurs in poorly specified rods, is typically in fatigue under the combined tensile and bending cycle rather than simple compression.

5. Interactive Calculator

Adjust the inputs below to explore how changes to engine specification affect peak force and stress. All calculations use the same two-term Fourier model as the study above.

6. Conclusions

01

Mass reduction works

The Wossner forged piston cuts 80 g from reciprocating mass per cylinder. At 8,500 rpm this translates to a 3,144 N reduction in peak inertia force — a 15.1% improvement.

02

Con-rod is adequately specified

Both OEM and modified configurations return a factor of safety above 2.0 against the rod material UTS in simple tension. The OEM rod is not the weak point at 8,500 rpm for inertia loading alone.

03

Piston speed is the limiting factor

Mean piston speed of 21.8 m/s approaches the practical limit for cast iron bores (~20 m/s). The switch to forged pistons and bore finishing was driven partly by this consideration.

04

Gas loads require separate analysis

These results cover inertia loading only. Peak combustion pressure (typically 60-80 bar for a naturally aspirated 1400) creates a compressive load on the rod during the power stroke that must be assessed separately for a complete fatigue life estimate.

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