Water Rocket
Computer Model Problems
Here is the third Water
Rocket Computer Model Problem.
The screen shot below is from the 3D optimisation of
the default 2 litre water rocket.
Again I have included the file details so that you can
reproduce it yourself to investigate the peculiar maxima
displayed in the screen shot on the right.
It is a plot of Distance Downrange as the output
variable with Angle of Elevation (39.3g to 47.9g) on the
Y axis and Mass of Rocket Empty (190.5g to 260.4g) on the
X axis with a post-thrust integration interval of 10ms.
The maximum shows a number of diagonal lines that run
all of the way across the display.
Variables |
Water Rocket Computer Model Problem 03 |
|
|
Rocket |
Mass of Rocket Empty |
120 |
|
g |
Capacity of Pressure Vessel |
2050 |
|
cm3 |
Rocket Diameter |
9.5 |
|
cm |
Rocket Coeff of Drag |
0.56 |
|
|
Nozzle Diameter |
21.5 |
|
mm |
Constant K for nozzle |
0.16 |
|
|
[ ] Launch Tube in use |
Not Used |
|
|
Duration of air impulse |
50 |
|
ms |
[ ] Parachute in use |
Not Used |
|
|
Launch
Tube |
Length |
20 |
|
cm |
External
Diameter |
21 |
|
mm |
[X] Hollow
Launch Tube |
Used |
|
|
Wall Thickness |
2 |
|
mm |
Length of Tube
Empty |
25 |
|
cm |
Distance of
Vent from End |
0 |
|
cm |
[ ] T-Nozzle
in use |
Not Used |
|
|
T-Nozzle
Diameter |
4.75 |
|
mm |
Parachute |
Diameter
opened out flat |
1.2 |
|
m |
Parachute
Coeff of Drag |
0.9 |
|
|
Deploy ()
Apogee.( ) Timer |
4 |
|
s |
Delay in
opening |
5 |
|
m |
Initial |
Mass of Water |
850 |
|
g |
Pressure in Vessel |
100 |
|
psi |
Height |
1.5 |
|
feet |
Angle of Elevation |
88 |
|
° |
Speed at Angle of Elevation |
0 |
|
m/s |
Temperature |
10 |
|
C |
Environmental |
Gamma of Gas in Rocket |
1.402 |
|
|
Density of Gas in Rocket |
1.293 |
|
kg/m3 |
Density of Liquid in Rocket |
998 |
|
kg/m3 |
Acceleration due to Gravity |
9.81 |
|
m/s2 |
Atmospheric Pressure |
1013 |
|
mBar |
Density of Air at STP |
1.293 |
|
kg/m3 |
The problem here
is . . . |
1. |
to
find an explanation for the diagonal lines. |
The variables are in the table on the left...
If you give up or you think you know what is going on,
look at the answers.
|