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Mathematica-Rocket equation - Repost

Instructions:

Produce a manipulate block that:

tory of of a rocket launched as time is varied.

Allows starting mass, fuel mass, burn rate and exhaust velocity to be set.

Displays current height, velocity and mass as time varies.

Gives a clear graphical representation of height, velocity and mass as time varies (2 marks)

t should be presented as a complete notebook, giving a brief description of the Kiolovsky rocket equation and how to interpret the graphic.

You should produce 3 modules:

Question 1: MaxHeight[eV_, rM_, fM_, bR_] which calculates the maximum height the rocket reaches given the paramters (1 mark)

Question 2: MaxVelocity[eV_, rM_, fM_, bR_]which calculates the maximum velocity the rocket reaches given the paramters (1 mark)

Question 3: FlightTime[eV_, rM_, fM_, bR_], which calculates the amount of time the rocket spend in the air (1 mark)

You should also produce a Manipulate block that produces a visulatisation of the rockets trajectory

Question 4: produce a Manipulate block that allows a user to manipulate the Exhaust Velocity, Rocket Mass, Fuel Mass, Burn Rate, and Time to view the trajectory of the rocket. (2 marks)

Habilidades: Matlab and Mathematica

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Acerca do Empregador:
( 1 comentário ) Perth, Australia

ID do Projeto: #5090665

Premiar a:

bchandra1955

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$54 AUD em 3 dias
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