Finding max. velocity of jet w/ constant and/or changing acceleration

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Homework Help Overview

The discussion revolves around evaluating the relationship between fuel consumption and the maximum attainable velocity of a jet fighter, considering different scenarios for the rate of fuel consumption as a function of time. The problem involves concepts from dynamics, specifically the application of force and acceleration equations.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • The original poster attempts to analyze three scenarios of fuel consumption and their impact on acceleration and maximum velocity. They express uncertainty about how to handle the changing rate of fuel consumption in situations two and three, and whether assumptions need to be made about the rate of decrease. Other participants question the implications of changing mass on the application of Newton's second law and discuss the relevance of momentum in this context.

Discussion Status

Participants are exploring various interpretations of the problem, particularly regarding the effects of changing mass on force calculations. Some guidance has been offered regarding the use of momentum, but there is no explicit consensus on the best approach to take. The original poster has requested assistance without seeking a complete solution, indicating an ongoing exploration of the topic.

Contextual Notes

The original poster notes the absence of initial conditions and expresses confusion about how to represent the changing rate of fuel consumption in their calculations. There is a suggestion that participants should start new threads if they seek further clarification or assistance.

mgsintheta
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Homework Statement



You must evaluate the relationship between fuel consumption and the attainable velocity of a new jet fighter. Given that:

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



If fjet=A(r(t))4/3,
then the Accelerationjet=[A(r(t))4/3]/m
-make A/m=C, then Accelerationjet=C[r(t)]4/3

Knowing that the integral of an acceleration should be the velocity function:
∫C[r(t)]4/3=C∫[r(t)]4/3→ C[(3/7)r(t)7/3+A]

My problem with the above is that I am not sure what to do about the constant. Does it matter? No initial conditions are given, so I don't believe that I can solve for it. If I was able to, it might be able to help me solve this problem.
Here is my dilemma. I understand that for situation 1, the acceleration is constant, and that I can use the constant-acceleration kinematics equation vf=vo+at. Since the acceleration is constant, the maximum velocity will be attained at the end of the acceleration period: 10C[550]4/3=45062.66988(A/m) However, for situations two and three, I am unsure of how to express the rate at which r(t) is decreasing, in order to be able to come up with a function that will give me the maximum velocity.
I understand that for situations 2 and 3, the maximum velocity will still be obtained at the end of the acceleration period. However, I am unsure of how to represent those answers differently than situation 1, as r(t) is constantly changing. I know that the graph of the acceleration vs. time graph for situation 2 is a straight diagonal line going down from left to right, and the graph for situation 3 is a concave up graph decreasing from left to right. Do I need to make an assumption about the rate of decrease for each of these situations? As in come up with a function to represent r(t) through the acceleration period? Or is there a way to come up with the maximum velocity concretely? I don't want the answer obviously, just some guidance to steer me towards that "aha" moment. Thanks for the assistance.
 
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If the fuel is consumed whether the mass of the jet remains constant ?
 
In the case when mass changes (because of fuel), F=ma no longer helps. Try F=dP/dt
 
what exactly is P?
 
mgsintheta said:
what exactly is P?
In F = dp/dt, p stands for momentum. But I disagree with davidchen9568. You can still use F=ma, provided you bear in mind that m is variable. Indeed, F = dp/dt can lead you astray when the mass is varying.
 
Can someone work the whole problem out. Still a little confused.
 
Noah Drakes said:
Can someone work the whole problem out. Still a little confused.
This is a very old thread (2013). The Original Poster was last logged on in 2015. It is unlikely that the OP will be back to engage in the thread.

I suggest that you start your own new thread and show the work you have done so far.
 

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