SFTY 335 Week 5 Assignment Help | Embry Riddle
- embry-riddle-aeronautical-university / SFTY 335
- 10 Jan 2020
- Price: $25
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· SFTY 335 Week 5 Assignment Help | Embry Riddle
Your case study is due at the end of the
module week.
Research two aircraft that are notably
different. Compare and contrast cost, performance, design, material selection,
and maintenance requirements. Estimate variables (e.g. cost) which aren’t
readily available. Where estimates are used, justify your thought process.
For one of the aircraft, discuss three design
features and associated tradeoffs (performance and/or structural) engineers
likely contemplated. For one of the tradeoffs, outline the pros and cons of the
decision.
Within your report, discuss the relationship
between aerodynamic performance and structural design and how each influences
one another.
For one of the aircraft, estimate the maximum
normal bending stress at the wing-fuselage interface using the following
simplifying assumptions:
1. There exists a primary spar carrying the
bending load.
2. The spar can be modeled as an “I-beam.”
3. Estimate a reasonable spar size (length,
depth, height) and material.
A. Note: You will need to look up the Modulus of Elasticity (“E”)
based upon your pick of the material you chose for your spar.
4. The “Second Moment of Area” (I) from our
stress equation, Stress = My/I, can be determined similar to the following
image, Figure 1.
https://erau.instructure.com/courses/104254/files/19811359/download
1. Figure
1. Stress equation for I-beam.
Please view detailed alt text for Figure
1. Stress equation for I-beam (DOCX).
2. The
only force acting on the wing is gravity (weight).
3. The
weight of the wing is distributed evenly across its length.
Based upon the spar material you selected, calculate the wing
spar Factor of Safety. Also, estimate the maximum wingtip deflection(𝛿max) based upon the case of a “Cantilever Beam with a Uniformly
Distributed load”as shown in these slides of Cantilever Beam
equations images (PPTX).
Within your report, show all calculations in an appendix,
discuss the findings, and comment on the reasonableness of the simplifying
assumptions.
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