AERO3261 - Aerospace Propulsion And Engine Matching Report Writing - Engineering Assignment Help

Assignment Task

You are a propulsion engineer in an aeronautical consultancy company. Your CEO has acquired a research contract from a UAV manufacturer who is looking to upgrade its engine and propeller. The engineers in the company are confused by the alleged claims of the advantages of one engine/ propeller combination over the other. Their confusion is further increased by the wide range of propellers that are available and you are tasked to shed light on the best propeller selection.

To do this your boss tasked you to perform an analysis to gain fundamental insight into the optimum propeller for this aircraft. The goal of your study is to determine the best propeller for this aircraft and set a standard against which the available propellers can be compared. You are given the following data to perform your task.

The assignment consists of 2 main parts:

1. Further develop the provided blade element code and simulate your propeller
2. Match the propeller to the provided engine data and to the aircraft under investigation

A more detailed description of what is required for each part follows next.

Part 1: Blade Element Code

For this part you are provided with a mostly populated “skeleton” of a blade element code. Most of the adjustments that need to be made to a standard blade element code are already there. The others are described here and comments are provided in the code to guide you as to where to insert them.

Part 2: Propeller – Engine – Airframe matching

The second part of the assignment consists of matching the engine and propeller combination with your airframe.

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