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Overview

This course introduces the fundamentals of aerodynamics, aircraft performance and stability. Students will be introduced to basic aeronautical concepts such as parts of the aircraft, properties of the atmosphere, altimetry and airspeed, lift and drag. Starting from the equations of continuity, momentum and energy, fluid flow equations for subsonic and … For more content click the Read More button below.  

Conditions for Enrolment

Prerequisite: ZPEM1302 or ZPEM1304

Delivery

In-person - Standard (usually weekly or fortnightly)

Fees

Pre-2019 Handbook Editions

Access past handbook editions (2018 and prior)