25-Nav-A1 Fundamentals of Naval Architecture · May-98-Nav-A1 2016
Question 4 of 7: Trim Angle of a Box Barge After Flooding One Compartment
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examinations, May 2016 — 98-Nav-A1 Fundamentals of Naval Architecture, 3 hours, closed book (5 questions constitute a complete exam paper, first five as they appear in the answer book are marked, each of equal value; all 7 answered below for full study coverage).
Reference texts: Tupper, Introduction to Naval Architecture; Lewis (ed.), Principles of Naval Architecture (PNA); IMO, International Code on Intact Stability (IS Code).
Question 4: Trim Angle of a Box Barge After Flooding One Compartment
Given. One of ten identical, previously-empty (permeability 100%) watertight compartments floods completely and remains open to the sea — solved by the lost-buoyancy method (constant displacement, intact waterplane provides all the buoyancy).
Plan view: 5 transverse sections (12 m each) × port/starboard (5.25 m each) = 10 compartments; one starboard-forward compartment is flooded.
Approach. Use the lost-buoyancy method: find the parallel rise from the volume lost up to the original draft over the intact waterplane area, locate the new centre of flotation, compute the intact waterplane's longitudinal inertia about it, then find the trimming moment produced by the lost buoyancy about the new $F$.
Waterplane areas. Each compartment is $60.00/5=12.0\text{ m}$ long by $10.50/2=5.25\text{ m}$ wide, area $=63.0\text{ m}^2$. Original waterplane $A_W=60.00(10.50)=630.0\text{ m}^2$, intact waterplane $A_W'=630.0-63.0=567.0\text{ m}^2$.
Parallel rise (constant-displacement/lost-buoyancy). Buoyancy lost up to the original draft: $v=63.0(3.00)=189.0\text{ m}^3$.
$$\text{rise}=\frac{v}{A_W'}=\frac{189.0}{567.0}=0.3333\text{ m}\ \Rightarrow\ T'=3.00+0.333\approx3.333\text{ m}$$
New centre of flotation. Taking $x$ positive forward from midship, the lost area's centroid is at $x_c=+24.0\text{ m}$:
$$x_F'=\frac{0(630.0)-24.0(63.0)}{567.0}\approx-2.667\text{ m (i.e. 2.667 m aft of midship)}$$
Intact waterplane's longitudinal inertia about the new $F$. Whole-box $I_L=\dfrac{BL^3}{12}=\dfrac{10.50(60.00)^3}{12}=189{,}000\text{ m}^4$ about midship. The lost compartment's own inertia is $\dfrac{5.25(12.0)^3}{12}=756.0\text{ m}^4$, so about midship it contributes $756.0+63.0(24.0)^2=37{,}044\text{ m}^4$. Intact $I_L$ about midship $=189{,}000-37{,}044=151{,}956\text{ m}^4$; shifting to the new centroid ($x_F'=-2.667\text{ m}$) by the parallel-axis theorem:
$$I_L'=151{,}956-567.0(-2.667)^2\approx147{,}924\text{ m}^4$$
Trimming moment and trim angle. $MCT1cm=\dfrac{\rho\,I_L'}{100L}=\dfrac{1.025(147{,}924)}{100(60.00)}\approx25.27\text{ tonnef}\cdot\text{m/cm}$. Lever between the lost buoyancy's centroid and the new $F$: $24.0-(-2.667)=26.67\text{ m}$.
$$\text{Trimming moment}=v\rho\,d=189.0(1.025)(26.67)\approx5166\text{ tonnef}\cdot\text{m}\ \Rightarrow\ COT=\frac{5166}{25.27}\approx204.4\text{ cm}=2.044\text{ m}$$
$$\boxed{\tan\theta_{trim}=\frac{2.044}{60.00}\approx0.03408\ \Rightarrow\ \theta_{trim}\approx1.95^\circ\text{ (by the head)}}$$