International Journal of Impact Engineering - Dimensionless formulae for penetration depth of concrete target impacted by a non-deformable projectile

Over six decades of ballistic testing have produced dozens of empirical formulae for concrete penetration — NDRC, Barr (UKAEA), ACE. All three share the same structural defects: unit-dependent coefficients that break when switching from SI to imperial, nose shape parameters assigned as discrete lookup values rather than computed from geometry, and calibration ranges limited to shallow impacts (\(0.6 < X/d < 2.0\) ) that collapse at deep penetration (\(X/d > 5\) ) with errors exceeding 20%.

Li & Chen (2003) resolved these defects by building on two independent pillars. The Buckingham Pi theorem reduces the 10 physical variables of the problem to three dimensionless groups: the impact factor \(I^*\) , the mass ratio \(\lambda\) , and the nose factor \(N^*\) . Dynamic cavity expansion theory (Forrestal & Luk 1988) then provides the axial force law — static confinement resistance plus inertial resistance — and introduces the empirical parameter \(S\) that bridges uniaxial compressive strength to effective confined resistance. Combining the two theories recombines the three Pi groups into two operational numbers, \(I\) and \(N\) , which govern the result entirely.

The outcome is two closed-form formulae — Eq. (15a) for shallow penetration, Eq. (15b) for deep — validated against approximately 130 data points covering \(X/d\) from 0.07 to 92.8.


Quick Example

Reference diagram — rigid projectile geometry, semi-infinite concrete target, and penetration depth X

4340-steel ogive projectile, CRH = 2, impacting 35 MPa concrete at 277 m/s. Data: Forrestal et al. (1994), Table 3, shot 14.

InputValue
Mass \(M\)0.906 kg
Diameter \(d\)26.9 mm
Nose typeOgive, CRH \(\psi = 2\)
Impact velocity \(V_0\)277 m/s
Compressive strength \(f_c\)35.2 MPa
Concrete density \(\rho_c\)2370 kg/m³

Penetration depth: \(X = 167\,\text{mm}\) (\(X/d = 6.21\) , deep regime) Test measurement: 173 mm. Model error: 3.4%. NDRC prediction: 137 mm. NDRC error: 20.5%.

The 26.9 mm ogive projectile at 277 m/s penetrates 167 mm into 35 MPa concrete — about 6.2 calibers. At this velocity the static resistance term accounts for 94% of the retarding force; the dynamic inertia term contributes only 6%. NDRC, calibrated on shallow impacts, underestimates by a factor that grows with penetration depth.

Pipeline summary:

NodeOperationKey output
0Validity check\(V_0 = 277\) m/s \(< 800\) m/s, rigid projectile
1Nose geometry\(N^* = 0.156\) , \(k = 2.030\)
2Target resistance\(S = 12\) (paper)
3Dimensionless numbers\(I = 8.455\) , \(N = 125.9\)
4Regime\(I = 8.455 > \pi k/4 = 1.571\) → deep penetration
5bEq. (15b)\(X/d = 6.21\)
6Dimensional output\(X = 167\,\text{mm}\)

Pipeline Overview

Block diagram of the concrete penetration depth pipeline — 7 nodes from nose geometry to depth X

The pipeline is sequential with one bifurcation. Nodes 0–3 are always executed. Node 4 selects the depth formula based on whether \(I\) exceeds the crater threshold \(\pi k/4\) . Node 5a (shallow) or 5b (deep) computes the dimensionless depth; Node 6 converts to metres or millimetres.

📄 Download: The A4 Ballistic Pipeline — slide deck (PDF) - A visual representation of the calculation

📄Download The Theory Behind the Calculation (PDF) — A visual walkthrough of the physics: from Buckingham Pi to cavity expansion to the final dimensionless equations.


Node 0 — Validity Pre-Check

Purpose. Verify that the model assumptions hold before computing. If a condition is violated, the pipeline emits a warning but does not block execution — the engineering judgement remains with the user.

InputSymbolUnit
Impact velocity\(V_0\)m/s
Shank diameter\(d\)m
Aggregate size (optional)\(a\)m
ConditionCriterionReference
Rigid (non-deformable) projectile\(V_0 \lesssim 800\,\text{m/s}\) for hardened steelPaper §2.1
Semi-infinite targetthickness \(\geq 3X\) — verify after calculationModel assumption
Normal incidenceimpact angle = 90°Model assumption
Aggregate small vs. diameter\(d/a \gg 1\) (ideally \(> 5\) )Paper §2.1
Light or no reinforcement\(< 1.5\%\) per directionPaper §2.1
OutputSymbol
Status (pass / warning list)

Node 1 — Nose Geometry

Purpose. Compute the nose shape factor \(N^*\) and the dimensionless crater depth \(k\) .

InputSymbolUnit
Nose typeflat / ogive / conical / spherical
Nose parameter\(\psi\)

Nose factor \(N^*\) — Eqs. (2), (3a)–(3c)

\(N^*\) is defined by a surface integral over the nose profile. For standard geometries the integral has closed form:

Nose type\(\psi\) definition\(N^*\) formulaRange
Flat\(1.0\)
OgiveCRH \(= R/d\)\(\dfrac{1}{3\psi} - \dfrac{1}{24\psi^2}\)\(0 < N^* < 0.5\)
Conical\(H/d\)\(\dfrac{1}{1 + 4\psi^2}\)\(0 < N^* < 1.0\)
Spherical\(r/d\)\(1 - \dfrac{1}{8\psi^2}\)\(0.5 < N^* < 1.0\)

\(N^*\) is a continuous function of geometry, not a discrete lookup. A lower value means a sharper, more penetration-efficient nose: flat nose \(N^* = 1.0\) , hemispherical \(N^* = 0.5\) , ogive CRH=2 \(N^* = 0.156\) , ogive CRH=4.5 \(N^* = 0.076\) .

Nose height \(H/d\)

Nose type\(H/d\)
Flat\(0\)
Ogive\(\sqrt{\psi - 1/4}\)
Conical\(\psi\)
Spherical\(\psi - \sqrt{\psi^2 - 1/4}\)

Crater depth parameter \(k\) — Eq. (25)

The crater–tunnel transition depth is the sum of the Prandtl plastic slip depth for a flat punch (\(0.707d\) ) and the nose height \(H\) :

\[\boxed{k = 0.707 + \frac{H}{d}}\]
Nose\(\psi\)\(k\)
Flat0.707
Hemispherical0.51.207
Ogive CRH=222.030
Ogive CRH=332.365
Ogive CRH=4.54.52.769
OutputSymbolUnit
Nose shape factor\(N^*\)
Dimensionless crater depth\(k\)

Node 2 — Target Resistance

Purpose. Compute the empirical constant \(S\) that scales the uniaxial compressive strength \(f_c\) to the effective resistance under dynamic triaxial confinement. \(S\) cannot be derived analytically; it is back-calculated from penetration tests and then fitted as a function of \(f_c\) .

InputSymbolUnit
Unconfined compressive strength\(f_c\)MPa

Two correlations are provided (\(f_c\) in MPa for both):

Original — Forrestal et al. (1994), Eq. (12):

\[S_{\text{orig}} = 82.6 \; f_c^{-0.544}\]

Simplified — Li & Chen (2003), Eq. (21):

\[S_{\text{simpl}} = 72.0 \; f_c^{-0.5}\]

The simplified form makes \(I\) proportional to \(f_c^{-1/2}\) , aligning with the \(f_c\) dependence in NDRC, Hughes and Chang and enabling direct comparison. For \(f_c > 30\,\text{MPa}\) the two correlations are practically equivalent.

Target resistance constant S vs compressive strength fc — Forrestal (1994) and Li & Chen (2003) correlations

\(f_c\) (MPa)\(S_{\text{orig}}\)\(S_{\text{simpl}}\)\(S\) (paper)
13.521.019.621
2315.515.015.2
35.212.712.112
62.89.29.1
977.27.37

For shot 14 (\(f_c = 35.2\,\text{MPa}\) , \(S = 12\) from Table 2), both correlations agree to within 0.7 units.

OutputSymbolUnit
Target resistance constant\(S\)

Node 3 — Dimensionless Numbers

Purpose. Compute the two numbers that govern the penetration depth.

InputSymbolUnit
Projectile mass\(M\)kg
Impact velocity\(V_0\)m/s
Shank diameter\(d\)m
Compressive strength\(f_c\)Pa
Concrete density\(\rho_c\)kg/m³
Nose factor (Node 1)\(N^*\)
Target resistance (Node 2)\(S\)

Intermediate quantities

Impact factor (Eq. 5):

\[I^* = \frac{M V_0^2}{d^3 f_c}\]

Mass ratio (Eq. 6):

\[\lambda = \frac{M}{\rho_c \, d^3}\]

Johnson damage number (Eq. 7, informational):

\[\Phi_J = \frac{I^*}{\lambda} = \frac{\rho_c V_0^2}{f_c}\]

\(\Phi_J\) depends only on velocity and target — not on the projectile. It classifies impact severity independently of the launcher.

Operational numbers

\[\boxed{I = \frac{I^*}{S} = \frac{M V_0^2}{S \, d^3 f_c}}\]

\(I\) is the ratio of projectile kinetic energy to the concrete’s effective absorption capacity (resistance under confinement, scaled by \(S\) , over volume \(d^3\) ).

\[\boxed{N = \frac{\lambda}{N^*} = \frac{M}{N^* \rho_c \, d^3}}\]

\(N\) combines relative projectile mass and nose sharpness. A heavy, sharp projectile has large \(N\) and penetrates more for equal \(I\) .

OutputSymbolUnit
Impact function\(I\)
Geometry function\(N\)
(Intermediate) impact factor\(I^*\)
(Intermediate) mass ratio\(\lambda\)
(Intermediate) Johnson number\(\Phi_J\)

Node 4 — Regime Selection

Purpose. Determine whether the projectile stops inside the crater or advances into the tunnel.

InputSymbolUnit
Impact function (Node 3)\(I\)
Crater depth (Node 1)\(k\)

The projectile exits the crater zone with residual velocity \(V_1 > 0\) if and only if \(I > \pi k / 4\) :

\[\text{If } I \leq \frac{\pi k}{4} \quad \Rightarrow \quad \textbf{shallow} \text{ — projectile stops in crater, use Eq. (15a)}\]
\[\text{If } I > \frac{\pi k}{4} \quad \Rightarrow \quad \textbf{deep} \text{ — projectile enters tunnel, use Eq. (15b)}\]
Output
Regime: shallow or deep
Threshold value \(\pi k / 4\)

Node 5a — Shallow Penetration — Eq. (15a)

Condition: \(X/d \leq k\) (projectile stops within the crater zone)

Derived from the energy balance \(X^2 = MV_0^2/c\) with the crater force constant \(c\) from the continuity condition at \(x = kd\) :

\[\boxed{\frac{X}{d} = \sqrt{\frac{4kI}{\pi} \cdot \frac{1 + k\pi/(4N)}{1 + I/N}}}\]

Consistency checks. At the regime boundary \(I = \pi k/4\) : the formula gives \(X/d = k\) , matching the deep formula below. For \(N \gg 1\) : reduces to Eq. (16a) of the paper. For \(N \gg 1\) and \(I/N \ll 1\) : reduces to \(X/d = \sqrt{4kI/\pi}\) , Eq. (17a).

Note on shallow correction. For \(X/d < 0.5\) the formula systematically overestimates (paper Fig. 11). The empirical correction Eq. (27) — \(\left(X/d\right)_{\text{corr}} = 1.628\,(X/d)^{2.789}\) — is available in the notebook as an opt-in flag. It is off by default: the correction was fitted on flat-nosed, low-energy data where scatter is large, and its applicability to other nose types is uncertain.

OutputSymbolUnit
Dimensionless penetration depth\(X/d\)

Node 5b — Deep Penetration — Eq. (15b)

Condition: \(X/d > k\) (projectile traverses the crater and bores a tunnel)

Derived by integrating the equation of motion \(MV\,dV/dx = -(\pi d^2/4)(Sf_c + N^*\rho_c V^2)\) from \(x = kd\) to \(x = X\) , then non-dimensionalising through \(I\) and \(N\) :

\[\boxed{\frac{X}{d} = \frac{2}{\pi} \, N \ln\!\left(\frac{1 + I/N}{1 + k\pi/(4N)}\right) + k}\]

Penetration depth grows logarithmically with \(I\) at fixed \(N\) — not linearly. Each additional unit of velocity buys progressively less depth.

Consistency checks. At the regime boundary \(I = \pi k/4\) : \(\ln(1) = 0\) , giving \(X/d = k\) — exact continuity with Eq. (15a). For \(N \gg 1\) : reduces to Eq. (16b). For \(N \gg 1\) and \(I/N \ll 1\) : reduces to \(X/d = k/2 + 2I/\pi\) , Eq. (17b).

OutputSymbolUnit
Dimensionless penetration depth\(X/d\)

Node 6 — Dimensional Output

Purpose. Convert \(X/d\) to physical depth and summarise all intermediate values.

\[X = \frac{X}{d} \times d\]

Report also: regime, \(I\) , \(N\) , \(k\) , \(S\) , \(I^*\) , \(\lambda\) , \(\Phi_J\) , and the semi-infinite check (\(3X\) minimum target thickness).


Numerical Verification — Shot 14

Forrestal et al. (1994), Table 3. Ogive CRH=2, \(f_c = 35.2\,\text{MPa}\) .

Input

QuantityValue
\(M\)0.906 kg
\(d\)0.0269 m
\(V_0\)277 m/s
Noseogive, \(\psi = 2\)
\(f_c\)35.2 MPa
\(\rho_c\)2370 kg/m³

Node 1

\[N^* = \frac{1}{3 \times 2} - \frac{1}{24 \times 4} = \frac{1}{6} - \frac{1}{96} = \frac{15}{96} = 0.15625 \quad (\text{paper: } 0.156) \checkmark\]
\[\frac{H}{d} = \sqrt{2 - 0.25} = \sqrt{1.75} = 1.3229 \qquad k = 0.707 + 1.323 = 2.030\]

Note: paper Tables 2–4 use \(k = 2\) (empirical value from Forrestal 1994). The tool uses \(k = 2.030\) from Eq. (25). For this verification, \(k = 2\) is used to reproduce the paper tables.

Node 2

\[S_{\text{simpl}} = 72.0 \times 35.2^{-0.5} = 12.13 \qquad S_{\text{paper}} = 12\]

Node 3

\[I^* = \frac{0.906 \times 277^2}{(0.0269)^3 \times 35.2 \times 10^6} = \frac{69\,537}{684.6} = 101.46 \quad (\text{paper: } 101.46) \checkmark\]
\[\lambda = \frac{0.906}{2370 \times (0.0269)^3} = \frac{0.906}{0.04609} = 19.65 \quad (\text{paper: } 19.64) \checkmark\]
\[I = \frac{101.46}{12} = 8.455 \quad (\text{paper: } 8.45) \checkmark \qquad N = \frac{19.64}{0.156} = 125.9 \quad (\text{paper: } 125.9) \checkmark\]
\[\Phi_J = \frac{101.46}{19.64} = 5.17 \quad (\Phi_J \gg 1 \text{: fully dynamic regime})\]

Node 4

\[\frac{\pi k}{4} = \frac{\pi \times 2}{4} = 1.571 \qquad I = 8.455 > 1.571 \quad \Rightarrow \quad \textbf{deep penetration}\]

Node 5b

\[\frac{I}{N} = \frac{8.455}{125.9} = 0.06716 \qquad \frac{k\pi}{4N} = \frac{2\pi}{4 \times 125.9} = 0.01248\]
\[\frac{1 + I/N}{1 + k\pi/(4N)} = \frac{1.06716}{1.01248} = 1.05400 \qquad \ln(1.05400) = 0.05261\]
\[\frac{2}{\pi} N = \frac{2}{\pi} \times 125.9 = 80.15 \qquad \frac{X}{d} = 80.15 \times 0.05261 + 2 = 4.217 + 2 = 6.217\]

Paper Table 2, shot 14: \(X/d_{\text{anal}} = 6.21\) ✓ — \(X/d_{\text{test}} = 6.43\)\(X/d_{\text{NDRC}} = 5.11\)

Node 6

\[X = 6.217 \times 26.9\,\text{mm} = \mathbf{167.2\,\text{mm}}\]

Test: 173 mm. Error: 3.4%. Semi-infinite check: \(3X = 502\,\text{mm}\) minimum target thickness.


Figures

Dimensionless penetration depth vs impact function I — parametric curves for N = 20 to 1500 (reproduces Fig. 3 of the paper)

For fixed \(N\) , \(X/d\) grows logarithmically with \(I\) in the deep regime. The shallow-to-deep transition (knee of each curve) shifts with \(k\) and \(N\) . The current case is marked in red.

Dimensionless penetration depth vs geometry function N — parametric curves for I = 10 to 200 (reproduces Fig. 4 of the paper)

For fixed \(I\) , deeper penetration results from a heavier, sharper projectile (large \(N\) ). The sensitivity to \(N\) decreases as \(I/N \to 0\) — for shot 14 (\(I/N = 0.067\) ) geometry contributes marginally and \(X/d\) is driven almost entirely by \(I\) .


How to Use the Notebook

The Python notebook implements the full pipeline (Nodes 0–6) and runs directly on Google Colab. No installation required: numpy and matplotlib are preinstalled.

Open in Colab

Modify only the INPUT PARAMETERS cell. Parameters:

ParameterVariableUnitNote
Projectile massMkg
Shank diameterdm
Impact velocityV0m/s
Nose typenose_type"flat", "ogive", "conical", "spherical"
Nose parameterpsiCRH for ogive, \(H/d\) for conical, \(r/d\) for spherical
Compressive strengthfcPae.g. 35.2e6 for 35.2 MPa
Concrete densityrho_ckg/m³
\(S\) correlationS_correlation"simplified" (default) or "original"
Shallow correctionapply_shallow_correctionFalse (default); enable for \(X/d < 0.5\)

Each node prints its full output — all intermediate values are visible.

Known limitations. The model requires: rigid (non-deformable) projectile — erosion becomes significant above ~800 m/s for hardened steel; semi-infinite target — rear boundary effects (scabbing, perforation) not modelled, verify thickness \(\geq 3X\) ; normal incidence — oblique impact not covered; unreinforced or lightly reinforced concrete (\(< 1.5\%\) per direction); aggregate size small relative to diameter (\(d/a > 5\) recommended, continuum assumption breaks down below \(d/a \approx 2\) ).


References

[1] Li QM, Chen XW (2003). Dimensionless formulae for penetration depth of concrete target impacted by a non-deformable projectile. Int. J. Impact Eng. 28, 93–116.

[2] Forrestal MJ, Altman BS, Cargile JD, Hanchak SJ (1994). An empirical equation for penetration depth of ogive-nose projectiles into concrete targets. Int. J. Impact Eng. 15(4), 395–405.

[3] Forrestal MJ, Luk VK (1988). Dynamic spherical cavity-expansion in a compressible elastic-plastic solid. ASME J. Appl. Mech. 55, 275–279.

[4] Sliter GE (1980). Assessment of empirical concrete impact formulas. ASCE J. Struct. Div. 106(ST5), 1023–1045.