Use red parameter Can I get a fully explained work for all the question parts Problem A: Analysis of light aircraft rudderudder of an aircraft is usually found at the tail and is responsible for allowing the pilot to controlw about the vertical axis. Figure 2 shows a typical rear setup of a small aircraft, with the rudderred in gold. During maintenance, one way of mounting the rudder is to place one edge on apivot, whilst attaching the other edge on the end of an operational cable. Figure 3 shows anple of such a setup.Figure 1.1: (a) Small aircraft. (b) Rear end of small aircraft, highlighting rudder.Operational Cabley = BxD (m)Fixed pivot (A)(a)C (m)Figure 1.2: Rudder mounted in maintenance position.ParameterRedBlue5102376344.5832.8844GroupMass (kg)ABC (m)D (m)Green154552.2361Aircraft RudderPurple205461.882Yellow Orange25306732781.661 1.486 Leeds International Study CentreFoundation Year Engineering, Science and ComputingIn your report you must include:(a) The free body diagram of the rudder.(b) If the maximum permissible load that the steel operational cable can handle is 3kN, determinewhether it can handle the load of the rudder or not.(c) Determine the resultant load on the fixed pivot (A) and the angle at which it acts.(d) If the thickness of the rudder is included, describe which method you would use to find thecentre of gravity? How would this value differ from the calculation using a lamina modellingassumption?

Answered: Image /qna-images/answer/31ee1123-420b-4860-b6cb-5269a9c7442e.jpg

3 3 Problem A: Analysis of light aircraft rudder udder of an aircraft is usually found at the tail and is responsible for allowing the pilot to control w about the vertical axis. Figure 2 shows a typical rear setup of a small aircraft, with the rudder red in gold. During maintenance, one way of mounting the rudder is to place one edge on a pivot, whilst attaching the other edge on the end of an operational cable. Figure 3 shows an ple of such a setup. Figure 1.1: (a) Small aircraft. (b) Rear end of small aircraft, highlighting rudder. Operational Cable y = Bx Aircraft Rudder

3 3 Problem A: Analysis of light aircraft rudder udder of an aircraft is usually found at the tail and is responsible for allowing the pilot to control w about the vertical axis. Figure 2 shows a typical rear setup of a small aircraft, with the rudder red in gold. During maintenance, one way of mounting the rudder is to place one edge on a pivot, whilst attaching the other edge on the end of an operational cable. Figure 3 shows an ple of such a setup. Figure 1.1: (a) Small aircraft. (b) Rear end of small aircraft, highlighting rudder. Operational Cable y = Bx Aircraft Rudder

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

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Concept explainers

Forming and Shaping

Metal forming is a category of metalworking process through which the material can be given the desired shape and size by subjecting it to plastic deformation, where the component undergoes bulk deformation process upon application of loads. Unlike the shearing and machining process, the material does not undergo up to a failure point as indicated in the stress-strain curve. Hence, the stresses induced during the forming process are greater than yield strength but less than the failure strength of the material. The process does not lead to the loss of material, so it can be said to be an economical process. During forming, the material is subjected to tensile forces, compressive forces, bending, and shearing loading conditions. The material should possess the property of ductility to undergo the forming process.

Question

Use red parameter Can I get a fully explained work for all the question parts

Problem A: Analysis of light aircraft rudder
udder of an aircraft is usually found at the tail and is responsible for allowing the pilot to control
w about the vertical axis. Figure 2 shows a typical rear setup of a small aircraft, with the rudder
red in gold. During maintenance, one way of mounting the rudder is to place one edge on a
pivot, whilst attaching the other edge on the end of an operational cable. Figure 3 shows an
ple of such a setup.
Figure 1.1: (a) Small aircraft. (b) Rear end of small aircraft, highlighting rudder.
Operational Cable
y = Bx
D (m)
Fixed pivot (A)
(a)
C (m)
Figure 1.2: Rudder mounted in maintenance position.
Parameter
Red
Blue
5
10
2
3
7
6
3
4
4.583
2.8844
Group
Mass (kg)
A
B
C (m)
D (m)
Green
15
4
5
5
2.2361
Aircraft Rudder
Purple
20
5
4
6
1.882
Yellow Orange
25
30
6
7
3
2
7
8
1.661 1.486

Leeds International Study Centre
Foundation Year Engineering, Science and Computing
In your report you must include:
(a) The free body diagram of the rudder.
(b) If the maximum permissible load that the steel operational cable can handle is 3kN, determine
whether it can handle the load of the rudder or not.
(c) Determine the resultant load on the fixed pivot (A) and the angle at which it acts.
(d) If the thickness of the rudder is included, describe which method you would use to find the
centre of gravity? How would this value differ from the calculation using a lamina modelling
assumption?

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