vi i. If V2=2V1, Find W. ii. What will be W if V2=4V1. iii. Use Matlab or excel to plot the Energy in the interval [0, 2n]

Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
icon
Related questions
Question

hi, I want the answer for the whole question please

Task 3
a. If the Pressure produced by the gas cylinder of the motor of the
rocket is governed by the below equation:
P = sin*(V)cos³(V)
3
And the energy is given by:
V2
W =
PdV
V1
i.
If V2=2V1, Find W.
ii.
What will be W if V2=4V1.
iii.
Use Matlab or excel to plot the Energy in the interval [0, 2n]
b. If the vibration at the boundaries of the piston of the motor is
given by:
v(t)
= at + b; a, b are constants, you may choose any integer
value not equal to zero for any of them.
v(t) = te(-t).
v(t) = 5sin(2wt) cos(4wt)
find the average and rms vibration for each case:
i.
ii.
ii.
T
Vavg
v(t)dt
T
Transcribed Image Text:Task 3 a. If the Pressure produced by the gas cylinder of the motor of the rocket is governed by the below equation: P = sin*(V)cos³(V) 3 And the energy is given by: V2 W = PdV V1 i. If V2=2V1, Find W. ii. What will be W if V2=4V1. iii. Use Matlab or excel to plot the Energy in the interval [0, 2n] b. If the vibration at the boundaries of the piston of the motor is given by: v(t) = at + b; a, b are constants, you may choose any integer value not equal to zero for any of them. v(t) = te(-t). v(t) = 5sin(2wt) cos(4wt) find the average and rms vibration for each case: i. ii. ii. T Vavg v(t)dt T
1
VRMS =
v²(t)dt
T
c. If the pressure P of the rocket's gas at an altitude z, temperature T
is decaying at a rate proportional to the current pressure. For the
given data derive an expression of the pressure as a function of
altitude. Explain why you used the positive or negative sign in your
derived expression.
i.
Evaluate P at z= 5000 m.
If the proportional constant =
RT
find the value of T used to
ii.
produce the data if g=9.81 m/s², R=287 J/(kgK).
Find the rate of change of P with respect to T @T=200K.
iii.
Altitude (z)
Pressure (kP)
500
18.362
1000
16.858
1500
15.477
2000
14.210
2500
13.046
3000
11.977
Transcribed Image Text:1 VRMS = v²(t)dt T c. If the pressure P of the rocket's gas at an altitude z, temperature T is decaying at a rate proportional to the current pressure. For the given data derive an expression of the pressure as a function of altitude. Explain why you used the positive or negative sign in your derived expression. i. Evaluate P at z= 5000 m. If the proportional constant = RT find the value of T used to ii. produce the data if g=9.81 m/s², R=287 J/(kgK). Find the rate of change of P with respect to T @T=200K. iii. Altitude (z) Pressure (kP) 500 18.362 1000 16.858 1500 15.477 2000 14.210 2500 13.046 3000 11.977
Expert Solution
steps

Step by step

Solved in 4 steps with 4 images

Blurred answer
Knowledge Booster
Perimeter
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, advanced-math and related others by exploring similar questions and additional content below.
Recommended textbooks for you
Advanced Engineering Mathematics
Advanced Engineering Mathematics
Advanced Math
ISBN:
9780470458365
Author:
Erwin Kreyszig
Publisher:
Wiley, John & Sons, Incorporated
Numerical Methods for Engineers
Numerical Methods for Engineers
Advanced Math
ISBN:
9780073397924
Author:
Steven C. Chapra Dr., Raymond P. Canale
Publisher:
McGraw-Hill Education
Introductory Mathematics for Engineering Applicat…
Introductory Mathematics for Engineering Applicat…
Advanced Math
ISBN:
9781118141809
Author:
Nathan Klingbeil
Publisher:
WILEY
Mathematics For Machine Technology
Mathematics For Machine Technology
Advanced Math
ISBN:
9781337798310
Author:
Peterson, John.
Publisher:
Cengage Learning,
Basic Technical Mathematics
Basic Technical Mathematics
Advanced Math
ISBN:
9780134437705
Author:
Washington
Publisher:
PEARSON
Topology
Topology
Advanced Math
ISBN:
9780134689517
Author:
Munkres, James R.
Publisher:
Pearson,