(FIRM) - Boat Design
Transcript of (FIRM) - Boat Design
FREE INTERNET ROWING MODEL(FIRM)
EXAMPLES: Single Sculls
March 25, 2015
FIRM IS RESEARCH CODE!
Please check all estimates generated by the programagainst experimental results before committing anytime or funds to your project as no liability can be
accepted by Cyberiad.
c©2015 Cyberiad
Contents
1 INTRODUCTION 1
2 W1x: Women’s Single Sculls 22.1 W1x exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
3 LW1x: Lightweight Women’s Single Sculls 8
4 M1x: Men’s Single Sculls 13
5 LM1x: Lightweight Men’s Single Scull 18
1 INTRODUCTION
Four single scull examples are included in this version of FIRM. More will be added in future versions.
1
2 W1x: Women’s Single Sculls
Many of the results for this sculler (who we have named Aage) have been used throughout the FIRM manual. Measuredvalues of rigging details, oar angles, gate normal forces, and her anthropometry were used as input to FIRM. Body angleregimes for three complete strokes were extracted from videos taken during the trial and these were used to constrain theangles predicted by the inverse kinematic procedures.
Table 1: Summary of experimental results for this simulation: number of strokes, stroke rate, non-dimensional pull phase duration(tp/ts), minimum hull velocity (Umin), maximum hull velocity (Umax), and mean hull velocity (U).
Item Value
Nstrokes 28Rate (spm) 35.111 ±0.214tp/ts 0.540 ±0.005Umin (ms−1) 3.288 ±0.063Umax (ms−1) 5.430 ±0.060
U (ms−1) 4.529 ±0.061
Table 1 summarises the main quantities relating to the simulation for this sculler. Values are given ± one standarddeviation.
Table 2: Experimental oar-related values for this simulation: minimum and maximum oar angles, and maximum gate normal force.
Port Oar Starboard OarName Min. Angle Max. Angle Max. FGn Min. Angle Max. Angle Max. FGn
(degrees) (degrees) (N) (degrees) (degrees) (N)
Aage -59.8±0.43 43.2±0.33 404.4±14.1 -56.4±0.38 44.5±0.42 387.0±16.0
A blade loss factor of kloss = 0.015 has been used to bring FIRM predictions in line with the experimental mean speedof U = 4.529ms−1. Given the many uncertainties, this small 1.5% reduction seems quite acceptable. (Instead of using theblade loss factor, we could have adjusted, for example, the oarhandle centre of effort, the viscous form factor, or the air dragcoefficients). A further justification for the small adjustments is that they are well within the standard deviations aroundthe means of the maximum gate normal forces given in Table 1.
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W1x: Aage Exp. Exp. Mean ± SD Pred. Crew
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ms-1
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t/ts
W1x: Aage Exp. Exp. Mean ± SD Pred. Crew
Figure 1: Hull propulsive acceleration and crew cg acceleration (left); hull velocity and crew cg velocity (right).
The hull propulsive acceleration is shown in the left panel of Fig. 1. Experimental data is shown as pink dots; the thickblack curve is the mean of the measured values and the thin lines are one standard deviation (SD) either side of the meancurve. The green curve is FIRM’s prediction.
The agreement is quite good, however, it should be kept in mind that it was achieved by using body angle regimesspecifically chosen to get that good agreement.
2
There is a small dip at about t/ts = 0.15 where the acceleration drops below zero. That, of course, must reduce theboat speed, and this can be seen as a corresponding dip in the right panel of the figure. The cause of the dip is mostprobably a question of rowing technique. FIRM has been able to reproduce the curve, but it cannot be used on its own tosuggest reasonable ways to correct the deficiency. That requires good coaching, and a more thorough biomechanical analysis.Kleshnev [?] has examined similar “double peaks” in boat acceleration.
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Forc
e (N
)
t/ts
W1x: Aage Fprop Fboat Fcrew -Fdrag Fsys
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Dra
g (N
)t/ts
W1x: Aage Air Viscous Wave Total
Figure 2: Equation of motion forces (left) and drag components (right).
The forces in the equations of motion are shown in the left panel of Fig. 2. Drag components during the stroke are inthe panel at the right.
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t/ts
W1x: Aage Exp. Port Exp. Star FIRM: Port FIRM: Star
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Join
t Ang
le (
degr
ees)
t/ts
W1x: Aage Knee Hip Neck Shoulder
Figure 3: Oar azimuth angles Ψxy (left); joint angles (right)).
Experimental oar azimuth angles in the plot at the left of Fig. 3 have been shifted so they are referenced to the centre ofthe pin. The continuous curves are the values used as input to FIRM.
Joint angle regimes are shown in the plot at the right of Fig. 3. Solid curves are the values used as input to FIRM.Gate normal forces are shown at the left of Fig. 4. The curves are the values used as input to FIRM.Oarblade propulsive forces are shown in the right panel of Fig. 4. These include the variation in the OBCP during the
stroke.The x-wise velocities of the OHCE are shown at the left of Fig. 5. The velocity is negative during the drive because the
handle travels in the negative x-direction.The seat velocity is shown in the right panel of Fig. 5. It too is negative during the pull phase. At the release the seat
velocity slows down and remains at zero for a short time before the stern is pulled towards the rower during the recovery.
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F Gn
(N)
t/ts
W1x: Aage Exp. Port Exp. Star FIRM: Port FIRM: Star
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F Bx
(N)
t/ts
W1x: Aage Port Star
Figure 4: Gate normal forces FGn (left); blade propulsive forces FBx (right).
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x-v
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m/s
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t/ts
W1x: Aage Port Star
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Seat
vel
ocity
(m
/s)
t/ts
W1x: Aage Hip (Seat)
Figure 5: OHCE horizontal velocity (left); seat velocity (right).
Yawing moment lever arms are shown in the left plot of Fig. 6. These, and the yawing moments shown at the right ofthe figure both contain the effects of the OBCP varying during the stroke.
Vertical oar angles are shown in the plot at the left of Fig. 7. The corresponding locations of the OBCP for both oarsare shown at the right. The vertical angles and vertical locations for both oars are identical, however, the azimuth angles aredifferent.
The OBCP is below the water from about t/ts = 0.01 to t/ts = 0.55. For the purposes of this plot, the OBCP is assumedto be at the geometric centre of the blade when it is out of the water.
The trajectories of the joints are shown in the plot at the left of Fig. 8; trajectories of the segment and oar centres ofgravity are shown at the right.
The trajectory of the hip is a flat line because it is the same as that of the seat which does not move up or down duringthe stroke. The trajectory of the sum of the CG is the black trace in the right-hand plot. It can be seen that the verticaldisplacement is much less than the horizontal which justifies ignoring the vertical component in many models.
The OBCP trajectories in Fig. 9 have been plotted on the same side of the hull for clarity and comparison. Puddles aremost likely to be formed during the period immediately before the release.
2.1 W1x exercises
Once we have good agreement between FIRM predictions of hull propulsive acceleration and hull velocity, there are manysimple “what if” type questions we can ask. Most of the short exercises can be done by making very simple modifications to
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W1x: Aage Port Star
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t/ts
W1x: Aage Port Star Sum
Figure 6: Yawing moment lever arms (left); yawing moments (right).
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t/ts
W1x: Aage Port Star
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z obc
p (m
. abo
ve w
ater
)
t/ts
W1x: Aage Waterplane Port OBCP Star OBCP
Figure 7: Vertical oar angles Ψyz (left); OBCP trajectories in the yz-plane (right).
one of the input files.Remember to restore the original value in the file before you try another example. The best method is to make a copy of
the line you want to modify, then use the # character to comment out the original line. After you finish the exercise, deletethe modified line, and remove the # character from the original line. (If you forget what modifications you made, delete theentire FIRM directory and re-install it: that should only take a few seconds.)
Before making any modifications to the files, run FIRM for the original file and record the mean hull velocity that appearson the Model Screen, or in the summary.csv file.
Exercise W1x 1.0: What is the predicted mean hull velocity at 20◦C water and 20◦C air temperature?Hint: change the values near the start of the main input file, aage.inExercise W1x 1.1: What difference in time over 2000m does the change in mean velocity represent?Exercise W1x 1.2: How many metres does the change in mean velocity represent?
Exercise W1x 2.0: When rowers resume training after a lay-off, they are usually not as strong as when they are at their peak.What is the effect of reducing the maximum gate forces by 10%? Hint: Change the blade loss factor.
Exercise W1x 3.0: Although the boat used in this example is very similar to the actual boat used in the on-water trials, itseems a little large for this rower. (Some people refer to this as “over-boating”). What is the effect of using a different hull,for example the slightly shorter S075L101g1 hull?Hint: change the line in the Hull Filename block of the file aage.in fromhulls/S080L106a1.csv
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W1x: Aage Knee Hip Neck Port Hand Star Hand
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x-ordinate of CG relative to ankle (m)
W1x: Aage Shank Thigh Torso Head Upper Arm Forearm Port Oar Star Oar Sum
Figure 8: Joint trajectories (left); trajectories of centres of gravity (right).
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om h
ull c
entr
elin
e (m
)
x (m)
Direction of
Boat Travel
Release
Catch
W1x: Aage Port Star
Figure 9: OBCP trajectories in the xy-plane.
tohulls/S075L101g1.csv
Exercise W1x 3.1: Examine the effect of changing the dimensions of the S080L106a1.csv hull. For example, change the lengthof the hull from 7.90 to 7.80. What is the effect on mean hull speed? How does it affect transverse stability (i.e. on GMT0)?
Exercise W1x 3.2: Make the S080L106a1.csv hull narrower by reducing the overall beam from 0.275m to 0.270m. What isthe effect on mean hull speed and transverse stability?
Exercise W1x 4.0: What is the effect on hull velocity of increasing the hull weight by 1, 2, or 3 kgs?Hint: change the values in the hull input file.
Exercise W1x 5.0: What is the effect of increasing the rower’s weight by 1, 2 and 3 kgs?Hint: change the values of the rower’s weight in the anthro.csv input file.Exercise W1x 5.1: Is the effect exactly the same as increasing the hull weight by the same amount, for example, by carryinglarge bottles of water?
Exercise W1x 6.0: Look up the world’s best time for this event in the Appendix to the FIRM manual. Now change the gateforces for this sculler, run FIRM and note the new mean hull velocity. What percentage increase in force is required for Aageto equal the world record time?
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W1x: AageRate 35.1 spmSpeed 4.53 m/s
Dead Mass 14.0 kgMoving Mass 76.2 kgTotal Mass 90.2 kgA.
MUSCULAREFFORT
398 W
100 %
NetKinetic Energy
Work onOarhandles
B.HANDLES
B/A
316 W
79 %
E.SYSTEMMOMENTUME/A
82 W
21 %
NOTE: B+F=D+H and C+E=D+G
C.PROPULSION
C/A
254 W
64 %
Blade EfficiencyC/B = 80.5 %
Propelling EfficiencyD/(D+H) = 83.6 %
F.FOOT BOARDS(External)F/A
59 W
15 %
Mom. EfficiencyF/E = 71.9 %
Work doneon shellD.
DRAG
D/A
313 W
79 %
AirVisc.Wave
11 % 82 % 7 %
Transferred to air and water
H.BLADELOSSESH/A
62 W
15 %Lost to water
G.BODY FLEX(Internal)G/A
23 W
6 %Lost as heat, breath etc.
Velocity Efficiency1-G/A = 94.2 %I=D+G+H.
TOTALLOSSI/A
398 W
100.0 %Net Efficiency
D/(D+H)-G/A = 77.8 %
Figure 10: Power flow chart.
7
3 LW1x: Lightweight Women’s Single Sculls
The on-water trial for this lightweight sculler, “Lara”, was conducted over 500m. Air and water temperatures were notrecorded: they were estimated as 10◦C and 10◦C respectively. Measured values of rigging details, oar angles, gate normalforces, and her anthropometry were used as input to FIRM. Body angle regimes were not recorded but were estimated bythe author using a complicated fitting process.
Table 3: Summary of experimental results for this simulation: number of strokes, stroke rate, non-dimensional pull phase duration(tp/ts), minimum hull velocity (Umin), maximum hull velocity (Umax), and mean hull velocity (U).
Item Value
Nstrokes 34Rate (spm) 27.902 ±0.248tp/ts 0.453 ±0.005Umin (ms−1) 2.861 ±0.030Umax (ms−1) 4.540 ±0.034
U (ms−1) 4.061 ±0.022
Table 3 summarises the main quantities relating to the simulation for this sculler. Values are given ± one standarddeviation.
Table 4: Experimental oar-related values for this simulation: Minimum and maximum oar angles, and maximum gate normal forceFgn.
Port Oar Starboard OarName Min. Angle Max. Angle Max. FGn Min. Angle Max. Angle Max. FGn
(degrees) (degrees) (N) (degrees) (degrees) (N)
Lara -62.9±1.19 43.2±0.48 354.3±10.4 -60.3±0.56 44.0±0.47 362.7±12.9
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LW1x: Lara Exp. Exp. Mean ± SD Pred. Crew
2.75
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U (
ms-1
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t/ts
LW1x: Lara Exp. Exp. Mean ± SD Pred. Crew
Figure 11: Hull propulsive acceleration and crew CG acceleration (left); hull velocity and crew CG velocity (right).
The hull propulsive acceleration is shown in the left panel of Fig. 11. Experimental data is shown as pink dots; the thickblack curve is the mean of the measured values and the thin lines are one standard deviation (SD) either side of the meancurve. The green curve is FIRM’s prediction.
The most notable feature of the hull speed curve in the plot at the right of Fig. 11 is the long, relatively constant regionduring the recovery. This behaviour is not evident in other classes of rowing; it might be peculiar to this particular lightweightsculler, or to lightweight women sculling at relatively low rates and with short drive phase durations.
The forces in the equations of motion are shown in the left panel of Fig. 12. Drag components during the stroke are inthe panel at the right.
Experimental oar azimuth angles and values used as input to FIRM are shown in the plot at the left of Fig. 13.Estimated joint angle regimes used as input to FIRM are shown in the plot at the right of Fig. 13.
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Forc
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LW1x: Lara Fprop Fboat Fcrew -Fdrag Fsys
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LW1x: Lara Air Viscous Wave Total
Figure 12: Equation of motion forces (left) and drag components (right).
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LW1x: Lara Exp. Port Exp. Star FIRM: Port FIRM: Star
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Join
t Ang
le (
degr
ees)
t/ts
LW1x: Lara Knee Hip Neck Shoulder
Figure 13: Oar azimuth angles Ψxy (left); joint angles (right)).
Gate normal forces are shown at the left of Fig. 14. The curves are the values used as input to FIRM.Oarblade propulsive forces are shown in the right panel of Fig. 14. These include the variation in the OBCP during the
stroke.The x-wise velocities of the OHCE are shown at the left of Fig. 15. The velocity is negative during the drive because the
handle travels in the negative x-direction.The seat velocity is shown in the right panel of Fig. 15. It too is negative during the pull phase. At the release the seat
velocity slows down and remains at zero for a very short time before the stern moves towards the rower during the recovery.Yawing moment lever arms are shown in the left plot of Fig. 16. These, and the yawing moments shown at the right of
the figure both contain the effects of the OBCP varying during the stroke. The nett yawing moment is quite small for thissculler.
Vertical oar angles are shown in the plot at the left of Fig. 17. The corresponding locations of the OBCP for both oarsare shown at the right. The vertical angles and vertical locations for both oars are identical, however, the azimuth angles aredifferent.
The OBCP is below the water from about t/ts = 0.01 to t/ts = 0.45; the latter value was specified in the main input file.For the purposes of this plot, the OBCP is assumed to be at the geometric centre of the blade when it is out of the water.The OBCP trajectories in Fig. 18 have been plotted on the same side of the hull for clarity and comparison. Puddles are
most likely to be formed during the period immediately before the release.
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LW1x: Lara Exp. Port Exp. Star FIRM: Port FIRM: Star
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F Bx
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LW1x: Lara Port Star
Figure 14: Gate normal forces (left); blade propulsive forces (right).
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LW1x: Lara Port Star
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LW1x: Lara Hip (Seat)
Figure 15: OHCE horizontal velocity (left); seat velocity (right).
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LW1x: Lara Port Star Sum
Figure 16: Yawing moment lever arms (left); yawing moments (right).
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LW1x: Lara Port Star
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p (m
. abo
ve w
ater
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LW1x: Lara Waterplane Port OBCP Star OBCP
Figure 17: Vertical oar angles Ψyz (left); OBCP trajectories in the yz-plane (right).
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e fr
om h
ull c
entr
elin
e (m
)
x (m)
Direction of
Boat Travel
Release
Catch
LW1x: Lara Port Star
Figure 18: OBCP trajectories in the xy-plane.
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LW1x: LaraRate 27.9 spmSpeed 4.07 m/s
Dead Mass 14.0 kgMoving Mass 62.0 kgTotal Mass 76.0 kgA.
MUSCULAREFFORT
268 W
100 %
NetKinetic Energy
Work onOarhandles
B.HANDLES
B/A
223 W
83 %
E.SYSTEMMOMENTUME/A
45 W
17 %
NOTE: B+F=D+H and C+E=D+G
C.PROPULSION
C/A
171 W
64 %
Blade EfficiencyC/B = 76.4 %
Propelling EfficiencyD/(D+H) = 79.5 %
F.FOOT BOARDS(External)F/A
35 W
13 %
Mom. EfficiencyF/E = 77.5 %
Work doneon shellD.
DRAG
D/A
205 W
77 %
AirVisc.Wave
11 % 81 % 9 %
Transferred to air and water
H.BLADELOSSESH/A
53 W
20 %Lost to water
G.BODY FLEX(Internal)G/A
10 W
4 %Lost as heat, breath etc.
Velocity Efficiency1-G/A = 96.2 %I=D+G+H.
TOTALLOSSI/A
268 W
100.0 %Net Efficiency
D/(D+H)-G/A = 75.8 %
Figure 19: Power flow chart.
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4 M1x: Men’s Single Sculls
The on-water trial for this sculler, “Stevo”, was conducted over 500m. Air and water temperatures were not recorded:they were estimated as 22◦C and 22◦C respectively. Measured values of rigging details, oar angles, gate normal forces, andhis anthropometry were used as input to FIRM. Body angle regimes for 2 complete strokes were extracted from videos takenduring the trial.
Table 5: Summary of experimental results for this simulation: number of strokes, stroke rate, non-dimensional pull phase duration(tp/ts), minimum hull velocity (Umin), maximum hull velocity (Umax), and mean hull velocity (U).
Item Value
Nstrokes 42Rate (spm) 34.991 ±0.205tp/ts 0.497 ±0.004Umin (ms−1) 3.431 ±0.079Umax (ms−1) 5.819 ±0.080
U (ms−1) 4.942 ±0.071
Table 5 summarises the main quantities relating to the simulation for this sculler. Values are given ± one standarddeviation.
Table 6: Experimental oar-related values for this simulation: Minimum and maximum oar angles, and maximum gate normal force.
Port Oar Starboard OarName Min. Angle Max. Angle Max. FGn Min. Angle Max. Angle Max. FGn
(degrees) (degrees) (N) (degrees) (degrees) (N)
Stevo -64.7±0.50 41.7±0.92 538.8±24.5 -61.3±0.55 43.3±0.49 602.9±26.9
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0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
a (g
)
t/ts
M1x: Stevo Exp. Exp. Mean ± SD Pred. Crew
3
3.5
4
4.5
5
5.5
6
6.5
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
U (
ms-1
)
t/ts
M1x: Stevo Exp. Exp. Mean ± SD Pred. Crew
Figure 20: Hull propulsive acceleration and crew cg acceleration (left); hull velocity and crew cg velocity (right).
The hull propulsive acceleration is shown in the left panel of Fig. 20. Experimental data is shown as pink dots; the thickblack curve is the mean of the measured values and the thin lines are one standard deviation (SD) either side of the meancurve. The green curve is FIRM’s prediction. Hull and crew CG velocities are shown at the right. Maximum gate normalforces were increased by 1% to make measured and predicted predicted mean velocity coincide more closely.
The forces in the equations of motion are shown in the left panel of Fig. 21. Drag components during the stroke are inthe panel at the right.
Experimental oar azimuth angles in the plot at the left of Fig. 22 have been shifted so they are referenced to the centreof the pin. The continuous curves are the values used as input to FIRM.
Gate normal forces are shown at the left of Fig. 23. The curves are the values used as input to FIRM.Oarblade propulsive forces are shown in the right panel of Fig. 23. These include the variation in the OBCP during the
stroke.
13
-300
-200
-100
0
100
200
300
400
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Forc
e (N
)
t/ts
M1x: Stevo Fprop Fboat Fcrew -Fdrag Fsys
0
20
40
60
80
100
120
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Dra
g (N
)
t/ts
M1x: Stevo Air Viscous Wave Total
Figure 21: Equation of motion forces (left) and drag components (right).
-80
-60
-40
-20
0
20
40
60
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
ψxy
(de
gree
s)
t/ts
M1x: Stevo Exp. Port Exp. Star FIRM: Port FIRM: Star
-60
-30
0
30
60
90
120
150
180
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Join
t Ang
le (
degr
ees)
t/ts
M1x: Stevo Knee Hip Neck Shoulder
Figure 22: Oar azimuth angles Ψxy (left); joint angles (right)).
The x-wise velocities of the OHCE are shown at the left of Fig. 24. The velocity is negative during the drive because thehandle travels in the negative x-direction.
The seat velocity is shown in the right panel of Fig. 24.Yawing moment lever arms are shown in the left plot of Fig. 25. These, and the yawing moments shown at the right of
the figure both contain the effects of the OBCP varying during the stroke.Vertical oar angles are shown in the plot at the left of Fig. 26. The corresponding locations of the OBCP for both oars
are shown at the right. The vertical angles and vertical locations for both oars are identical, however, the azimuth angles aredifferent.
The OBCP is below the water from about t/ts = 0.01 to t/ts = 0.497. For the purposes of this plot, the OBCP is assumedto be at the geometric centre of the blade when it is out of the water.
The OBCP trajectories in Fig. 27 have been plotted on the same side of the hull for clarity and comparison.
14
0
100
200
300
400
500
600
700
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
F Gn
(N)
t/ts
M1x: Stevo Exp. Port Exp. Star FIRM: Port FIRM: Star
0
50
100
150
200
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
F Bx
(N)
t/ts
M1x: Stevo Port Star
Figure 23: Gate normal forces FGn (left); blade propulsive forces FBx (right).
-3
-2
-1
0
1
2
3
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
OH
CE
x-v
eloc
ity (
m/s
)
t/ts
M1x: Stevo Port Star
-2
-1.5
-1
-0.5
0
0.5
1
1.5
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Seat
vel
ocity
(m
/s)
t/ts
M1x: Stevo Hip (Seat)
Figure 24: OHCE horizontal velocity (left); seat velocity (right).
-3
-2
-1
0
1
2
3
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Yaw
ing
mom
ent l
ever
arm
(m
)
t/ts
M1x: Stevo Port Star
-500
-400
-300
-200
-100
0
100
200
300
400
500
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Yaw
ing
Mom
ent (
Nm
)
t/ts
M1x: Stevo Port Star Sum
Figure 25: Yawing moment lever arms (left); yawing moments (right).
15
0
2
4
6
8
10
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
ψyz
(de
gree
s)
t/ts
M1x: Stevo Port Star
-0.2
-0.1
0
0.1
0.2
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
z obc
p (m
. abo
ve w
ater
)t/ts
M1x: Stevo Waterplane Port OBCP Star OBCP
Figure 26: Vertical oar angles Ψyz (left); OBCP trajectories in the yz-plane (right).
1.6
1.8
2
2.2
2.4
2.6
2.8
-2.8 -2.6 -2.4 -2.2 -2 -1.8 -1.6 -1.4 -1.2
Lat
eral
dis
tanc
e fr
om h
ull c
entr
elin
e (m
)
x (m)
Direction of
Boat Travel
Release
Catch
M1x: Stevo Port Star
Figure 27: OBCP trajectories in the xy-plane.
16
M1x: StevoRate 35.0 spmSpeed 4.94 m/s
Dead Mass 14.0 kgMoving Mass 97.9 kgTotal Mass 111.9 kgA.
MUSCULAREFFORT
578 W
100 %
NetKinetic Energy
Work onOarhandles
B.HANDLES
B/A
462 W
80 %
E.SYSTEMMOMENTUME/A
116 W
20 %
NOTE: B+F=D+H and C+E=D+G
C.PROPULSION
C/A
360 W
62 %
Blade EfficiencyC/B = 77.9 %
Propelling EfficiencyD/(D+H) = 81.4 %
F.FOOT BOARDS(External)F/A
88 W
15 %
Mom. EfficiencyF/E = 75.8 %
Work doneon shellD.
DRAG
D/A
448 W
77 %
AirVisc.Wave
10 % 82 % 8 %
Transferred to air and water
H.BLADELOSSESH/A
102 W
18 %Lost to water
G.BODY FLEX(Internal)G/A
28 W
5 %Lost as heat, breath etc.
Velocity Efficiency1-G/A = 95.2 %I=D+G+H.
TOTALLOSSI/A
578 W
100.0 %Net Efficiency
D/(D+H)-G/A = 76.6 %
Figure 28: Power flow chart.
17
5 LM1x: Lightweight Men’s Single Scull
The on-water trial for this lightweight sculler, “Karl”, was conducted over 500m during an early autumn morning.Measured values of rigging details, oar angles, gate normal forces, and his anthropometry were used as input to FIRM.Body angle regimes were not recorded but were estimated by the author using a complicated fitting process. Air and watertemperatures were not recorded: they were estimated as 10◦C and 15◦C respectively. A 1.155 ms−1 head wind has beenassumed.
Table 7: Summary of experimental results for this simulation: number of strokes, stroke rate, non-dimensional pull phase duration(tp/ts), minimum hull velocity (Umin), maximum hull velocity (Umax), and mean hull velocity (U).
Item Value
Nstrokes 25Rate (spm) 34.272 ±0.269tp/ts 0.545 ±0.005Umin (ms−1) 3.374 ±0.055Umax (ms−1) 5.487 ±0.060
U (ms−1) 4.529 ±0.054
Table 7 summarises the main quantities relating to the simulation for this sculler. Values are given ± one standarddeviation.
Table 8: Experimental oar-related values for this simulation: Minimum and maximum oar angles, and maximum gate normal forceFgn.
Port Oar Starboard OarName Min. Angle Max. Angle Max. FGn Min. Angle Max. Angle Max. FGn
(degrees) (degrees) (N) (degrees) (degrees) (N)
Karl -64.5±0.76 45.0±0.68 461.3±16.0 -58.9±0.85 47.7±0.57 439.0±11.6
A useful exercise would be to set the wind speed to zero and kloss to about 0.06. The mean hull speed for that caseshould be similar to the one where a head wind was used.
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
0.4
0.6
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
a (g
)
t/ts
LM1x: Karl Exp. Exp. Mean ± SD Pred. Crew
3
3.5
4
4.5
5
5.5
6
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
U (
ms-1
)
t/ts
LM1x: Karl Exp. Exp. Mean ± SD Pred. Crew
Figure 29: Hull propulsive acceleration and crew CG acceleration (left); hull velocity and crew CG velocity (right).
The hull propulsive acceleration is shown in the left panel of Fig. 29. Experimental data is shown as pink dots; the thickblack curve is the mean of the measured values and the thin lines are one standard deviation (SD) either side of the meancurve. The green curve is FIRM’s prediction.
The forces in the equations of motion are shown in the left panel of Fig. 30. Drag components during the stroke are inthe panel at the right.
Experimental oar azimuth angles and values used as input to FIRM are shown in the plot at the left of Fig. 31.Estimated joint angle regimes used as input to FIRM are shown in the plot at the right of Fig. 31.
18
-300
-200
-100
0
100
200
300
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Forc
e (N
)
t/ts
LM1x: Karl Fprop Fboat Fcrew -Fdrag Fsys
0
20
40
60
80
100
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Dra
g (N
)
t/ts
LM1x: Karl Air Viscous Wave Total
Figure 30: Equation of motion forces (left) and drag components (right).
-80
-60
-40
-20
0
20
40
60
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
ψxy
(de
gree
s)
t/ts
LM1x: Karl Exp. Port Exp. Star FIRM: Port FIRM: Star
-60
-30
0
30
60
90
120
150
180
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Join
t Ang
le (
degr
ees)
t/ts
LM1x: Karl Knee Hip Neck Shoulder
Figure 31: Oar azimuth angles Ψxy (left); joint angles (right)).
Gate normal forces are shown at the left of Fig. 32. The curves are the values used as input to FIRM.Oarblade propulsive forces are shown in the right panel of Fig. 32. These include the variation in the OBCP during the
stroke.The x-wise velocities of the OHCE are shown at the left of Fig. 33. The velocity is negative during the drive because the
handle travels in the negative x-direction. The seat velocity is shown in the right panel.Yawing moment lever arms are shown in the left plot of Fig. 34. These, and the yawing moments shown at the right of
the figure both contain the effects of the OBCP varying during the stroke. The nett yawing moment is quite small for thissculler.
Vertical oar angles are shown in the plot at the left of Fig. 35. The corresponding locations of the OBCP for both oarsare shown at the right. The vertical angles and vertical locations for both oars are identical, however, the azimuth angles aredifferent.
The OBCP is below the water from about t/ts = 0.01 to t/ts = 0.54; the latter value was specified in the main input file.For the purposes of this plot, the OBCP is assumed to be at the geometric centre of the blade when it is out of the water.The OBCP trajectories in Fig. 36 have been plotted on the same side of the hull for clarity and comparison.
19
-100
0
100
200
300
400
500
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
F Gn
(N)
t/ts
LM1x: Karl Exp. Port Exp. Star FIRM: Port FIRM: Star
-25
0
25
50
75
100
125
150
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
F Bx
(N)
t/ts
LM1x: Karl Port Star
Figure 32: Gate normal forces (left); blade propulsive forces (right).
-3
-2
-1
0
1
2
3
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
OH
CE
x-v
eloc
ity (
m/s
)
t/ts
LM1x: Karl Port Star
-1.5
-1
-0.5
0
0.5
1
1.5
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Seat
vel
ocity
(m
/s)
t/ts
LM1x: Karl Hip (Seat)
Figure 33: OHCE horizontal velocity (left); seat velocity (right).
-3
-2
-1
0
1
2
3
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Yaw
ing
mom
ent l
ever
arm
(m
)
t/ts
LM1x: Karl Port Star
-400
-300
-200
-100
0
100
200
300
400
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Yaw
ing
Mom
ent (
Nm
)
t/ts
LM1x: Karl Port Star Sum
Figure 34: Yawing moment lever arms (left); yawing moments (right).
20
0
2
4
6
8
10
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
ψyz
(de
gree
s)
t/ts
LM1x: Karl Port Star
-0.1
-0.05
0
0.05
0.1
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
z obc
p (m
. abo
ve w
ater
)t/ts
LM1x: Karl Waterplane Port OBCP Star OBCP
Figure 35: Vertical oar angles Ψyz (left); OBCP trajectories in the yz-plane (right).
1.6
1.8
2
2.2
2.4
2.6
-2.8 -2.6 -2.4 -2.2 -2 -1.8 -1.6 -1.4 -1.2
Lat
eral
dis
tanc
e fr
om h
ull c
entr
elin
e (m
)
x (m)
Direction of
Boat Travel
Release
Catch
LM1x: Karl Port Star
Figure 36: OBCP trajectories in the xy-plane.
21
LM1x: KarlRate 34.3 spmSpeed 4.53 m/s
Dead Mass 14.0 kgMoving Mass 75.0 kgTotal Mass 89.0 kgA.
MUSCULAREFFORT
436 W
100 %
NetKinetic Energy
Work onOarhandles
B.HANDLES
B/A
347 W
80 %
E.SYSTEMMOMENTUME/A
89 W
20 %
NOTE: B+F=D+H and C+E=D+G
C.PROPULSION
C/A
269 W
62 %
Blade EfficiencyC/B = 77.7 %
Propelling EfficiencyD/(D+H) = 81.2 %
F.FOOT BOARDS(External)F/A
65 W
15 %
Mom. EfficiencyF/E = 72.6 %
Work doneon shellD.
DRAG
D/A
334 W
77 %
AirVisc.Wave
17 % 77 % 6 %
Transferred to air and water
H.BLADELOSSESH/A
77 W
18 %Lost to water
G.BODY FLEX(Internal)G/A
24 W
6 %Lost as heat, breath etc.
Velocity Efficiency1-G/A = 94.4 %I=D+G+H.
TOTALLOSSI/A
436 W
100.0 %Net Efficiency
D/(D+H)-G/A = 75.6 %
Figure 37: Power flow chart.
22