I have uploaded 3 files the first one is the actual Satelloon project and the second one is the Outline that i did with the feedback of my teacher at the last 2 slides. the last file is the Marking Criteria. If you have any questions or need any help you can ask me.
Category: Aerospace Engineering
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Title: Strengths and Weaknesses of a Research Paper: A Critical Analysis Strengths of the Research Paper: 1. Clear and Concise Research Question: The research paper had a well-defined and focused research question that guided the entire study
What were the strengths of the research paper?
What were the weaknesses or areas that could have been improved?
What did you learn from their research? What can you contribute to their research? This can be an additional resource for the literature review, support for their recommendation, or another element that they could have considered during the research process.
You must include a properly formatted APA in-text citation and reference to support your contribution. -
Title: Compressor Performance Analysis and Comparison of Velocity Triangles at Different Locations in an Axial Compressor
This problem is a slight variation of the one we worked out in class. Suppose that air at 101.3 kP a
and 288 K enters an axial compressor with a velocity of 170 m/s. Assume, as we did in class, that air
enters and leaves a compressor stage along the axial direction, and further that the velocity at the exit of
the stator is identical to the velocity at the inlet of the rotor. Let the hub and tip diameters be 0.457 m and
0.66 m, respectively, and let the rotors rotate at 8000 rpm. The air is turned by 15◦ as it passes through
the rotor blades. Note that these are exactly the same values as the problem we worked out in class. In
class, we computed the velocity triangles by focusing on the mid-section of the rotor and stator. Compute
the velocity triangles instead at the hub. Compute the compressor work and stage pressure ratio using
the velocity triangle computed at the hub. Repeat the same calculations (velocity triangles, compressor
work, and stage pressure ratio), but this time at the tip of the rotor and stator blades. Compare the values
you obtain, and those we obtained in class, and comment on what you observe. You can assume that
air is an ideal gas, and that R = 287.16 J/kg/K, and γ = 1.4.
I attached the values obtained in the class. Please don’t use chatgpt because it’s giving wrong values even the premium one. Please make sure you know the correct solution before taking the job. i found a solution on chegg but I’m pretty sure it’s not that accurate.