Finding velocity with constant, incre., decrea, varying acce

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SUMMARY

The discussion focuses on calculating the maximum velocity of a fighter jet based on varying fuel consumption rates, represented as r(t). The three scenarios analyzed include constant, decreasing, and varying rates of fuel consumption, starting at 500 fighter fuel units (ffu) per minute over a 10-minute acceleration period. The relationship between force, mass, and acceleration is established using the equation F=ma, leading to the derived acceleration formula a=(A(r(t)^4/3)/m). The user seeks a detailed solution to the problem, emphasizing the need for step-by-step guidance.

PREREQUISITES
  • Understanding of Newton's Second Law (F=ma)
  • Familiarity with calculus, specifically differentiation
  • Knowledge of fuel consumption metrics in aviation (fighter fuel units)
  • Basic principles of kinematics related to acceleration and velocity
NEXT STEPS
  • Study the implications of varying fuel consumption on jet performance
  • Learn about the mathematical modeling of acceleration in physics
  • Explore the concept of drag force and its effects on velocity
  • Investigate advanced calculus techniques for solving differential equations
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in performance optimization of aircraft dynamics will benefit from this discussion.

Noah Drakes
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Homework Statement



Force of jet= A(r(t))4/3
A: constant determined by the fighter model in the class being considered and the drag force on the plane
r(t): the rate of fuel consumption as a function of time

Consider 3 possible situations for r(t):

1. when the rate is constant for the duration of the acceleration period
2. when the rate is steadily decreasing for the duration of the acceleration period
3. when the rate decreases at a decreasing rate as the plane accelerates

For each of these you should assume that the rate is initially 500 ffu (fighter fuel units)/min,
and for each it is reasonable to suppose an acceleration period of 10 minutes.

Determine-in terms of the characteristics of the fighter (m and A)- the maximum velocity obtained by the jet

Homework Equations



F=ma

The Attempt at a Solution



I set F=ma equal to Fjet = A(r(t)^4/3. So ma=A(r(t)^4/3 .

Now i solved for "a" to get an equation for acceleration: a=(A(r(t)^4/3)/(m)

Then i differentiated the equation to get velocity : A/m * 3/7 (r(t) ^ (7/3)

confused on how to approach the problem from here. I have a test on wednesday with a problem similar to this problem. It would be immensly helpful if someone solved the problem explaining each step and why.

I am new to this community by the way.
 
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i also want to point out i copied the question from someone else's forum, but the work is mine.
 

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