Compressible Flow and Propulsion 2

Overview

Following a review of fundamental thermodynamics, relationships for 1D isentropic compressible flows are derived.

Principles of normal/oblique shockwaves & Prandtl-Meyer Expansion fans are introduced, extended to analysis of nozzle/diffuser configurations. Shock-Expansion theory & Ackerets theory are also introduced. This is extended to analysis of common Aerospace propulsion methods, reviewing historical developments in Aerospace propulsion focussing on the thermodynamic models of the jet engine.

Content covers 1st/2nd laws of thermodynamics, Joule Cycle, basic analysis of gas turbine cycles and review of the design of gas turbine components.

Learning Objectives

Apply knowledge of mathematics, statistics, natural science and engineering principles to the solution of complex problems. Some of the knowledge will be at the forefront of the particular subject of study.

Analyse complex problems to reach substantiated conclusions using first principles of mathematics, statistics, natural science and engineering principles.

Select and evaluate technical literature and other sources of information to address complex problems.

Function effectively as an individual, and as a member or leader of a team.

Communicate effectively on complex engineering matters with technical and non-technical audiences.

Select and critically evaluate technical literature and other sources of information to solve complex problems.

Function effectively as an individual, and as a member or leader of a team. Evaluate effectiveness of own and team performance.

Communicate effectively on complex engineering matters with technical and non-technical audiences, evaluating the effectiveness of the methods used.

Skills

Analyse data using appropriate techniques.

Demonstrate analytical and problem-solving skills.

Manage time effectively in order to achieve intended goals.

Participate effectively in the operation of a team and collaborate effectively with members of the team.

Assessment

None.