This project was aligned to examine two model aircraft wings, each designed for different primary operating speeds. The wings were tested in a wind tunnel at varying speeds and angles of attack, and the given results showed data typical of what would be expected when comparing a full-scale Boeing 707 to a Concorde. It also gives a good account of the unique lift characteristics of the Concorde wing.

This experiment aims to analyze the aerodynamic performance of model wings based on those of the Concorde and Boeing 707 aircraft. By subjecting these model wings to varying wind speeds and angles of attack in a wind tunnel, we aim to measure the lift and drag forces generated and understand how different wing shapes influence aerodynamic characteristics. This project also has stake in the improvement of environmental sustainability - increasing aircraft efficiency by way of optimizing lift produced whilst also minimizing drag promises to reduce given emissions created by engines, leading to less fuel consumption and improved greenhouse gas emissions rates for all flying aircraft today.

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