An aircraft wing spar made of aluminum alloy has an I-beam cross-section and is subjected to a bending moment due to aerodynamic lift. Given the spanwise bending moment distribution, how would you determine the maximum bending stress in the spar? Also, explain how material fatigue considerations affect the design.
Technical questions related to Mtech project Thermodynamic cycles Recent advancements in IC engines Challenges faced in the experimental work How did you fix it
Why are you interested in NREL
Structural Analysis - ARCH and Cable RCC - Shear and Footing Design
Explain why you think you are a good fit for this position and what you can bring to the job environment
They asked about my past work
Are you okay with handling radioactive materials?
What is your favorite algorithm.
What do your peers view as your strengths and weaknesses? Followed immediately by what you view as your strengths and weaknesses.
During the phone interview, they asked me to describe my previous research experience. The in-person interview was mostly them asking if I was able to complete specific tasks that would be included in the position and why I was interested in the position.
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