AERODYNAMICS 2 - 2020/1
Module code: ENG3207
In light of the Covid-19 pandemic, and in a departure from previous academic years and previously published information, the University has had to change the delivery (and in some cases the content) of its programmes, together with certain University services and facilities for the academic year 2020/21.
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This third year module in Aerospace Engineering is lecture- and tutorial- based, and continues to develop the understanding of aircraft aerodynamics and design started in ENG2089, ENG2091 and ENG3067 by concentrating on the prediction of lift in compressible flow, the characteristics of hypersonic flow, the impact of these topics on the design of supersonic aircraft, and experimental methods fluid mechanics.
Mechanical Engineering Sciences
BIRCH David (Mech Eng Sci)
Number of Credits: 15
ECTS Credits: 7.5
Framework: FHEQ Level 6
JACs code: H400
Module cap (Maximum number of students): N/A
Prerequisites / Co-requisites
Completion of the progress requirements of Level FHEQ5, together with ENG3167 (Aerodynamics I)
Indicative content includes:
Compressible flow theory – nozzle flows, normal and oblique shock waves, expansion waves, the shock-expansion theory, viscous flow and heat transfer.
Design of supersonic aircraft - history, wing design, aircraft design for fully supersonic flight.
Hypersonic flow – characteristics of hypersonic flow, gas dynamics, Newtonian and related theories.
Experimental methods – wind tunnels for low and high-speed flow, measurement techniques, experimental methods, related applications.
|Assessment type||Unit of assessment||Weighting|
|School-timetabled exam/test||Class test (40 mins)||20|
The assessment strategy is designed to provide students with the opportunity to demonstrate understanding of scientific principles, the ability to adapt and apply those principles to specific calculations and the ability to describe aspects of aerodynamic phenomena and aircraft design. The class test demonstrates the ability to perform a specific calculation and interpret its results.
The summative assessment for this module consists of:
Examination (Learning outcomes 1-7) 2 hours (80%)
In-semester test (Learning outcome 1) 40 mins (20%)
Coursework as an alternative to the class test for late summer assessment (20%)
Formative assessment and feedback
Verbal feedback and discussion are provided during tutorial classes
Written feedback is provided on the class test
Feedback is also provided via material on SurreyLearn
- To provide an understanding of methods for predicting nozzle flows, and lift and wave drag in supersonic flow, including the effects of finite aspect ratio.
- To demonstrate how these strands are brought together through a broad discussion of the design of supersonic aircraft.
- To provide a general appreciation of the physics of hypersonic flow and simple methods for estimating lift in hypersonic flows.
- To provide an understanding of the specialist experimental facilities and instrumentation used in fluid mechanics, both for aeronautical and related applications.
|001||Understand and be able to apply theories for predicting the behaviour of compressible flows in ducts and nozzles||CK||SM1B/M, SM2B/M, EA1B/M|
|002||Understand and be able to apply theories for predicting lift and wave drag on finite aspect ratio wings in supersonic flight||CK||SM1B/M, SM2B/M, EA1B/M|
|003||Demonstrate a comprehensive understanding of the underlying theoretical basis of the methods used||K||SM1B/M|
|004||Understand and be able to apply knowledge acquired to the general design of supersonic aircraft||CK||SM1B/M, SM2B/M, EA1B/M|
|005||Understand the nature of hypersonic flow and be able to apply simple theoretical models for lift estimation||CK||SM1B/M, SM2B/M, EA1B/M|
|006||Understand the design and operation of the main classes of experimental facility and the associated instrumentation||KT||EA1B/M, EA2, P2/M,|
|007||Be aware of non-aeronautical applications||K||SM3B/M|
C - Cognitive/analytical
K - Subject knowledge
T - Transferable skills
P - Professional/Practical skills
Overall student workload
Independent Study Hours: 110
Lecture Hours: 30
Tutorial Hours: 10
Methods of Teaching / Learning
The learning and teaching strategy is designed to develop subject knowledge through theory, applications and worked examples. The module content is delivered through lectures, tutorial classes and SurreyLearn material.
The learning and teaching methods include three hours of lectures per week for ten weeks, one hour of tutorials for ten weeks and eight hours of revision classes.
Indicated Lecture Hours (which may also include seminars, tutorials, workshops and other contact time) are approximate and may include in-class tests where one or more of these are an assessment on the module. In-class tests are scheduled/organised separately to taught content and will be published on to student personal timetables.
Indicated Lecture Hours (which may also include seminars, tutorials, workshops and other contact time) are approximate and may include in-class tests where one or more of these are an assessment on the module. In-class tests are scheduled/organised separately to taught content and will be published on to student personal timetables, where they apply to taken modules, as soon as they are finalised by central administration. This will usually be after the initial publication of the teaching timetable for the relevant semester.
Reading list for AERODYNAMICS 2 : http://aspire.surrey.ac.uk/modules/eng3207
Programmes this module appears in
Please note that the information detailed within this record is accurate at the time of publishing and may be subject to change. This record contains information for the most up to date version of the programme / module for the 2020/1 academic year.