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Flight Testing / Modeling |
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Aim To compare the flight of the water rockets and ballista bolts used in the second impact comparison test. |
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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. |
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Results | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
The results of the flight testing for the water rockets and ballista bolts are show below. | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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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:
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.
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