Project

Inclining Experiment and Lightship Verification Project

Naval engineering project for planning and reducing an inclining experiment, including draft and density correction, pendulum readings, GM calculation, free-surface correction, KG update, uncertainty checks, and handover evidence.

This project produces an inclining-experiment and lightship verification package for a small vessel after construction changes. The objective is to determine whether the vessel’s measured displacement and vertical center of gravity are consistent with the stability documentation used for operation.

An inclining experiment is not only a calculation of metacentric height. It is a controlled measurement exercise. Draft readings, water density, loose weights, slack tanks, mooring forces, wind, pendulum geometry, test-weight positions, and onboard condition all affect the result.

Project Objective

Plan, execute, and reduce a simplified inclining experiment for a workboat after a deck-crane upgrade and machinery-room modification.

The deliverable must include:

  • test condition and exclusions;
  • draft, trim, and water-density correction;
  • test-weight shift log;
  • pendulum readings and heel angles;
  • observed metacentric height;
  • free-surface correction;
  • updated lightship KG;
  • comparison with design estimate;
  • uncertainty and acceptance statement;
  • handover actions for the stability booklet or loading computer.

Test Boundary

Use this representative vessel condition:

QuantityValue
vessel typesmall workboat
hydrostatic displacement from draft curves at reference density522.5\ \text{t}
reference seawater density1.025\ \text{t/m}^3
measured harbor water density1.020\ \text{t/m}^3
hydrostatic transverse metacentric height referenceuse KM_T from curves
KM_T at test displacement5.20\ \text{m}
design lightship displacement estimate512\ \text{t}
design lightship KG estimate3.66\ \text{m}
residual free-surface correction0.06\ \text{m}

The experiment uses movable test weights. Tanks are either pressed full, empty, or documented. Loose gear is secured or removed. Mooring lines are slack enough not to restrain heel, and wind conditions are recorded.

Acceptance Criteria

Use these acceptance criteria for the project review:

CheckAcceptance criterion
difference between measured and estimated lightship displacement\le 2.0\% or engineering disposition
difference between measured and estimated KG\le 0.10\ \text{m} or stability model update
pendulum repeatabilityreadings within 5\ \text{mm} for repeated equivalent shifts
heel angle rangelarge enough for measurement, small enough for small-angle assumptions
free-surface statecontrolled, documented, and corrected
final evidencesufficient for stability documentation update

These criteria are project screening values. Real vessel acceptance must follow the applicable class, flag, owner, and regulatory procedure.

Step 1: Correct Displacement for Water Density

The draft readings are reduced using hydrostatic curves prepared for reference seawater density:

\rho_{ref}=1.025\ \text{t/m}^3

The curve gives:

\Delta_{ref}=522.5\ \text{t}

The measured harbor density is:

\rho_{test}=1.020\ \text{t/m}^3

Correct the displacement:

\displaystyle \Delta=\Delta_{ref}\frac{\rho_{test}}{\rho_{ref}}
\displaystyle \Delta=522.5\frac{1.020}{1.025}=519.95\ \text{t}

Use:

\Delta=520\ \text{t}

Engineering Comment

Density correction matters because the same draft does not imply the same displacement in fresh, brackish, and seawater. A small density error can become a significant weight error when the vessel displacement is large.

Step 2: Record Weight Shift and Pendulum Data

Use one test weight:

w=3.0\ \text{t}

The transverse shift distance is:

d=6.0\ \text{m}

Pendulum length:

L=3.0\ \text{m}

Recorded deflections for equivalent port and starboard shifts are:

RunDeflection
172\ \text{mm}
275\ \text{mm}
373\ \text{mm}
474\ \text{mm}

Average deflection:

\displaystyle x_{avg}=\frac{72+75+73+74}{4}=73.5\ \text{mm}

Convert to meters:

x_{avg}=0.0735\ \text{m}

For small heel angles:

\displaystyle \tan\theta\approx\frac{x}{L}

Therefore:

\displaystyle \tan\theta=\frac{0.0735}{3.0}=0.0245

Engineering Comment

The repeated readings are close enough for a screening reduction. If port and starboard results were asymmetric, the team would investigate mooring restraint, wind, hull contact, pendulum friction, loose liquid, or a test-weight position error before accepting the data.

Step 3: Calculate Observed GM

The inclining moment is:

M=w d
M=3.0(6.0)=18.0\ \text{t m}

For a small heel angle:

\displaystyle GM_{obs}=\frac{w d}{\Delta\tan\theta}

Substitute the measured values:

\displaystyle GM_{obs}=\frac{18.0}{520(0.0245)}
\displaystyle GM_{obs}=\frac{18.0}{12.74}=1.41\ \text{m}

Engineering Comment

This is the observed metacentric height under the test condition. It reflects the vessel, the test loading, and any free-surface effects present during the experiment. It is not yet the clean lightship vertical center of gravity.

Step 4: Apply Free-Surface Correction

A residual slack tank cannot be fully pressed or emptied for the test. Its calculated free-surface correction is:

FSC=0.06\ \text{m}

The solid-condition metacentric height is:

GM_{solid}=GM_{obs}+FSC
GM_{solid}=1.41+0.06=1.47\ \text{m}

Engineering Comment

Free surface reduces observed stability. When deriving the vessel’s solid-condition lightship KG, the correction is added back to the observed GM. For loading-condition checks with slack tanks, the correction is subtracted from the uncorrected GM of that condition.

Step 5: Derive Lightship KG

From the hydrostatic curves at the corrected test displacement:

KM_T=5.20\ \text{m}

The relationship is:

GM=KM-KG

Therefore:

KG=KM_T-GM_{solid}
KG=5.20-1.47=3.73\ \text{m}

The measured lightship vertical center of gravity is:

KG_{meas}=3.73\ \text{m}

Engineering Comment

The result is a vessel property only if the test condition has been reduced correctly. Temporary loads, missing stores, unrecorded tools, trapped water, and onboard personnel must be accounted for in the lightship correction.

Step 6: Compare with Design Estimate

Measured displacement:

\Delta_{meas}=520\ \text{t}

Design estimate:

\Delta_{design}=512\ \text{t}

Difference:

\Delta W=520-512=8\ \text{t}

Percent difference:

\displaystyle \frac{8}{512}(100)=1.56\%

Measured KG:

KG_{meas}=3.73\ \text{m}

Design KG estimate:

KG_{design}=3.66\ \text{m}

Difference:

\Delta KG=3.73-3.66=0.07\ \text{m}

Both differences are within the project screening criteria:

1.56\%<2.0\%
0.07\ \text{m}<0.10\ \text{m}

Engineering Comment

The measured vessel is heavier and has a slightly higher KG than the design estimate. The difference is small enough to accept after engineering review, but the stability documentation should use the measured values rather than the older estimate.

Step 7: Check Measurement Uncertainty

Assume pendulum deflection uncertainty:

\delta x=\pm2\ \text{mm}

Relative deflection uncertainty:

\displaystyle \frac{\delta x}{x}=\frac{2}{73.5}=0.0272=2.72\%

Because:

\displaystyle GM\propto\frac{1}{x}

the deflection contribution to relative GM uncertainty is approximately:

\displaystyle \frac{\delta GM}{GM}\approx2.72\%

For:

GM_{obs}=1.41\ \text{m}

the deflection-related uncertainty is:

\delta GM\approx0.0272(1.41)=0.038\ \text{m}

Use a rounded screening uncertainty:

GM_{obs}=1.41\pm0.04\ \text{m}

Engineering Comment

This is not a full uncertainty budget. A formal reduction should also consider weight calibration, shift distance, draft readings, water density, hydrostatic interpolation, tank state, mooring restraint, wind, and pendulum alignment. The simple check shows that the KG margin is not dominated by one unreadable pendulum measurement.

Failure Modes to Control

Failure modeEffect on resultControl
slack tank not correctedKG appears too low or too high depending on reduction methodtank status log and free-surface correction
mooring line restrains heelmeasured deflection is too small, GM appears too highslack mooring check and repeat shifts
test weight position errorinclining moment is wrongmarked deck positions and survey measurement
wind gust during readinginconsistent pendulum dataweather limit and repeated readings
unrecorded onboard weightslightship displacement and KG are biasedweight survey and removal/addition log
wrong water densitydisplacement is biasedhydrometer or density measurement record

Handover Package

The final deliverable should contain:

  1. vessel identification, test date, location, weather, water density, and responsible engineer;
  2. test condition drawing or table showing all onboard weights and tank states;
  3. draft readings, trim, hydrostatic interpolation, and density correction;
  4. test-weight certification and measured shift distances;
  5. pendulum geometry, raw readings, averaged deflections, and heel calculation;
  6. observed GM, free-surface correction, corrected GM, and derived KG;
  7. comparison with design lightship estimate and disposition of differences;
  8. uncertainty notes and rejected readings, if any;
  9. stability-booklet or loading-computer update requirement;
  10. sign-off by naval architecture, operations, and owner or class representative as applicable.

Decision

The project result is acceptable for the screening criteria:

  • displacement difference is below 2 percent;
  • KG difference is below 0.10 m;
  • pendulum readings are repeatable;
  • free-surface correction is documented;
  • measured values should replace the design estimate in the stability record.

The vessel should not rely on the older lightship estimate after the modification. The correct engineering action is to update the stability documentation with the measured displacement and KG, preserve the inclining evidence, and require a new review after any future modification that changes weight, vertical center of gravity, tank configuration, or operating envelope.

REF

See also