11. If a wing construction does not have a rib, what failure will likely to occur? A creep B buckling C crushing D fatigue 12. What load is a tie rod designed to accept? a. Tension b. Shear C. Torsion d. compression|
11. If a wing construction does not have a rib, what failure will likely to occur? A creep B buckling C crushing D fatigue 12. What load is a tie rod designed to accept? a. Tension b. Shear C. Torsion d. compression|
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
Related questions
Question
![11. If a wing construction does not have a rib, what failure will likely to occur?
А creep
B buckling
Cc crushing
D fatigue
12. What load is a tie rod designed to accept?
а.
Tension
Shear
Torsion
b.
С.
d.
compression|
13. What other longitudinal member supports longerons in fuselage construction?
14. Which of the following choices is true about box beams? (1) closed section box beams is
used in aircraft wings (ii) closed section box beams is capable of resisting torsional loads
Both (1) and (ii) are false
Both (i) and (ii) are true and (ii) is not the correct reason for (i)
() is true but (ii) is false
Both (1) and (i) are true and (i) is the correct reason for (i)
а.
b.
С.
d.
15. stringers are used in monocoque type of fuselage construction
True
False
16. Why are aluminum alloys used on aircraft, instead of pure aluminum?](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F63565f9b-0a6c-4771-85c0-4b400c1d98d8%2F77838e0c-08a9-4914-a7de-645e3301820b%2Fc1htbob_processed.png&w=3840&q=75)
Transcribed Image Text:11. If a wing construction does not have a rib, what failure will likely to occur?
А creep
B buckling
Cc crushing
D fatigue
12. What load is a tie rod designed to accept?
а.
Tension
Shear
Torsion
b.
С.
d.
compression|
13. What other longitudinal member supports longerons in fuselage construction?
14. Which of the following choices is true about box beams? (1) closed section box beams is
used in aircraft wings (ii) closed section box beams is capable of resisting torsional loads
Both (1) and (ii) are false
Both (i) and (ii) are true and (ii) is not the correct reason for (i)
() is true but (ii) is false
Both (1) and (i) are true and (i) is the correct reason for (i)
а.
b.
С.
d.
15. stringers are used in monocoque type of fuselage construction
True
False
16. Why are aluminum alloys used on aircraft, instead of pure aluminum?
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