Battleships! In 1905, as part of the Russo-Japanese War, the Imperial Japanese Navy (IJN) under the command of Admiral Togo engaged the Russian fleet under the command of Admiral Rozhestvensky in the Battle of Tsushima. This was the first major naval engagement to be dominated by "big guns." In this question we will model the 12" Armstrong Whitworth guns employed by the IJN. The guns are capable of firing a 390kg shell at a speed of 732ms-1. For simplicity, we shall assume that this shell is a sphere of diameter D such that the drag due to air resistance can be approximated as Fp 2 CppAv² 16PDu² = cv? where Cp= 1/2 is the approximate drag coefficient for a sphere, A = T(D/2)2 is the reference area, p ~ 1.225kgm-3 is the density of air at sea level, and v is the velocity, whence C = 16PD? The overall force experienced by our shell in flight is hence F = mg - cv²v , where m is the mass of the shell and g is the acceleration due to gravity, v= and v^ = v/v, with v corresponding to the velocity vector. We shall take our coordinate system such that x^ points east, y^ points north, and z^ points up whence g-9.81z^. With this, let our gun be placed at the origin of our coordinate system, and assume our ship is at rest. We shall model the ship we are trying to hit with our shell as having a length of 121m, a beam of 23m, and being purely rectangular in shape. At t = 0 let the midpoint of this ship be located 4km to the north and 6km to the east of us, steaming with a speed of 7.5ms-1 in a south-southeast direction.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
icon
Related questions
Question
Battleships! In 1905, as part of the Russo-Japanese War, the Imperial Japanese Navy (IJN) under the
command of Admiral Togo engaged the Russian fleet under the command of Admiral Rozhestvensky
in the Battle of Tsushima. This was the first major naval engagement to be dominated by "big guns."
In this question we will model the 12" Armstrong Whitworth guns employed by the IJN.
The guns are capable of firing a 390kg shell at a speed of 732ms-1. For simplicity, we shall assume
that this shell is a sphere of diameter D such that the drag due to air resistance can be
approximated as
1
FD
CopAv²
where Cp = 1/2 is the approximate drag coefficient for a sphere, A = T(D/2)2 is the reference area, p
- 1.225kgm-3 is the density of air at sea level, and v is the velocity, whence
C =
16
pD?
The overall force experienced by our shell in flight is hence
F = mg – cvv ,
where m is the mass of the shell and g is the acceleration due to gravity, v= v and v^ = v/v, with
v corresponding to the velocity vector.
We shall take our coordinate system such that x^ points east, y points north, and z^ points up
whence g--9.81z^. With this, let our gun be placed at the origin of our coordinate system, and
assume our ship is at rest. We shall model the ship we are trying to hit with our shell as having a
length of 121m, a beam of 23m, and being purely rectangular in shape. At t = 0let the midpoint of
this ship be located 4km to the north and 6km to the east of us, steaming with a speed of 7.5ms-1 in
a south-southeast direction.
Transcribed Image Text:Battleships! In 1905, as part of the Russo-Japanese War, the Imperial Japanese Navy (IJN) under the command of Admiral Togo engaged the Russian fleet under the command of Admiral Rozhestvensky in the Battle of Tsushima. This was the first major naval engagement to be dominated by "big guns." In this question we will model the 12" Armstrong Whitworth guns employed by the IJN. The guns are capable of firing a 390kg shell at a speed of 732ms-1. For simplicity, we shall assume that this shell is a sphere of diameter D such that the drag due to air resistance can be approximated as 1 FD CopAv² where Cp = 1/2 is the approximate drag coefficient for a sphere, A = T(D/2)2 is the reference area, p - 1.225kgm-3 is the density of air at sea level, and v is the velocity, whence C = 16 pD? The overall force experienced by our shell in flight is hence F = mg – cvv , where m is the mass of the shell and g is the acceleration due to gravity, v= v and v^ = v/v, with v corresponding to the velocity vector. We shall take our coordinate system such that x^ points east, y points north, and z^ points up whence g--9.81z^. With this, let our gun be placed at the origin of our coordinate system, and assume our ship is at rest. We shall model the ship we are trying to hit with our shell as having a length of 121m, a beam of 23m, and being purely rectangular in shape. At t = 0let the midpoint of this ship be located 4km to the north and 6km to the east of us, steaming with a speed of 7.5ms-1 in a south-southeast direction.
d?
xx
C
C
-9.81-–viz î
VXX
vyy
m
m
m
(c) Assuming our gun is directed with an azimuthal angle p to thex-axis and an elevation of 0 such
that it makes a polar angle of T/2 – 0 with the z-axis, state the six initial conditions for our
system of ODES.
Hint: Recall that our gun is positioned at the origin and that our shells have an initial
velocity of 732ms-1,
(d) Given values of 0 and p we may begin to numerically solve our system of ODES. State the
termination condition for our simulation; that is to say at what time t should we stop running
our solver?
Transcribed Image Text:d? xx C C -9.81-–viz î VXX vyy m m m (c) Assuming our gun is directed with an azimuthal angle p to thex-axis and an elevation of 0 such that it makes a polar angle of T/2 – 0 with the z-axis, state the six initial conditions for our system of ODES. Hint: Recall that our gun is positioned at the origin and that our shells have an initial velocity of 732ms-1, (d) Given values of 0 and p we may begin to numerically solve our system of ODES. State the termination condition for our simulation; that is to say at what time t should we stop running our solver?
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 2 steps with 2 images

Blurred answer
Knowledge Booster
Applied Fluid Mechanics
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY