The module will be delivered with a blend of lectures, tutorials and problem-based learning with laboratory sessions, and individual self-directed research. This will include case study exercises and demonstration videos.
Module Aim:
The aim of this module is to introduce learners to the fundamental theories that form the basis of evaluating an aircraft's performance, and apply techniques to predict and analyse performance in various stages of flight.
Learning Outcomes
On successful completion of this module the learner should be able to:
LO1
Assess the atmospheric properties that influence aircraft performance.
LO2
Formulate the equations of motion for an aircraft in 2D flight.
LO3
Apply mathematical models to different phases of flight, and identify the inherent assumptions and limitations.
LO4
Analyse aircraft performance predictions using computer simulation techniques.
Pre-requisite learning
Module Recommendations
This is prior learning (or a practical skill) that is recommended before enrolment in this module.
No recommendations listed
Incompatible Modules
These are modules which have learning outcomes that are too similar to the learning outcomes of this module.
No incompatible modules listed
Co-requisite Modules
No Co-requisite modules listed
Requirements
This is prior learning (or a practical skill) that is mandatory before enrolment in this module is allowed.
No requirements listed
Module Content & Assessment
Indicative Content
The ISA
• relative density, pressure and temperature • the equation of state • the hydrostatic equation • Mach number, equivalent airspeed, calibrated airspeed, true airspeed.
Weight Performance
• aircraft mass estimation • wing loading • range and endurance calculations.
Drag
• maximum lift to drag ratio • minimum drag and minimum power airspeeds • plot the Drag Polar (Appendix 2 to CS23).
Engine Performance
• general engine performance • determine fuel flows and specific fuel values • derive and calculate the propulsive efficiency • understand thrust and power characteristics.
Performance
• aircraft ceiling • important airspeeds • limiting factors on flight envelopes (CS23.333) • corner velocities • accelerated stall lines • structural limits • cruise performance • specific range and endurance • take-off distance (CS23.59) • landing distance (CS23.75).
Manoeuvres
• stall speed (CS23.39) • speed stability • load factor • max load factor in a turn (V-N Diagram) (CS23.337) • climbing flight • turning performance • gliding performance.
• flight testing in a simulator • flight testing in a real live aircraft • flight test planning • test data capture • performance prediction.
Assessment Breakdown
%
Continuous Assessment
10.00%
Practical
30.00%
End of Module Formal Examination
60.00%
Continuous Assessment
Assessment Type
Assessment Description
Outcome addressed
% of total
Assessment Date
Examination
Students will be expected to sit one or more individual written assessments throughout the academic year, typically at the conclusion of one or more learning outcomes.
1,2,3
10.00
Week 7
No Project
Practical
Assessment Type
Assessment Description
Outcome addressed
% of total
Assessment Date
Practical/Skills Evaluation
Students will carry out a number of laboratory sessions throughout the academic year to enhance their understanding of the module, and will produce written reports describing each one. Laboratory practical work will include investigation of the following topics: flight performance estimation and analysis; computer simulation tools and mathematical modelling; real time flight analysis. It is envisaged that a number of these laboratory sessions will take place in both a simulated and a live aircraft flight environment.
1,2,3,4
30.00
Every Second Week
End of Module Formal Examination
Assessment Type
Assessment Description
Outcome addressed
% of total
Assessment Date
Formal Exam
Students will sit a formal written examination at the end of the semester.
1,2,3
60.00
End-of-Semester
SETU Carlow Campus reserves the right to alter the nature and timings of assessment