Flight

Testing / Modeling

This Section is Incomplete, Sorry

Aim

To compare the flight of the water rockets and ballista bolts used in the
second impact comparison test.
   
  Method

The water rockets and ballista bolts used in the second impact comparison test were fired from the cannon and ballista shown below at a number of different angles. The angle, time of flight and range for each shot were recorded.
   
 

Ballista

Cannon

   
  Results
   
  The results of the flight testing for the water rockets and ballista bolts are show below.
 
 
Water Rocket

46 Degrees

30 Degrees

15 Degrees

Range

Time

Range

Time

Range

Time

71

4.22

65

2.87

54

1.89

80

4.77

67

3.31

49

2.07

71

4.63

80

3.89

61

2.38

66

4.55

80

4.03

50

2.06

60

3.17

70

3.98

52

2.08

Average

69.6

4.28

72.4

3.6

53.2

2.01



Ballista

17 Degrees

27.5 Degrees

35 Degrees

Range

Time

Range

Time

Range

Time

40

1.7

57

2.65

55

3.02

42

1.75

56

2.84

52

2.64

54

2.67

Average

41

1.72

54.75

2.7

55

3.02

   
 

Discussion

To help compare the flight characteristics of the water rockets and ballista bolts a mathematical model was used. The model calculates the trajectory of a missile based on the following variables:

  • Mass
  • Angle of Elevation
  • Time of flight
  • Range
  • Initial velocity
  • Coefficient of friction

The first four variables can be fairly simply measured. The last two variables can be inferred by choosing values for them that cause the flight path generated by the model to most closely match an actual flights measured range and duration. A genetic algorithm was used to select the values for initial velocity and coefficient of friction that most matched the flight of each type of missile.

The results of the modeling are compared, in the table below, with the average measured values for each elevation used. Also shown are values of initial velocity and coefficient of friction used by the model along with the simulated energy and momentum of each missile once it had traveled a distance of 5 m.

Water Rocket - Modeled vs. Measured Values
Average

69.6

4.28

72.4

3.6

53.2

2.01

Modeled

68.8

4.64

72.4

3.4

54.0

1.88

Modeled Initial Velocity 38.3 m / s Kinetic Energy @ 5 meters 97 Joules
Modeled Friction Coefficient 0.04069 Momentum @ 5 meters 5.3 kg m / s

Ballista - Modeled vs. Measured Values
Average

41

1.72

54.75

2.7

55

3.02

Modeled

40.1

1.72

52.25

2.6

55.2

3.17

Modeled Initial Velocity 30.5 m / s Kinetic Energy @ 5 meters 156 Joules
Modeled Friction Coefficient 0.08992 Momentum @ 5 meters 10.7 kg m / s

This Section is Incomplete, Sorry

This Section is Incomplete, Sorry

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