This module will provide students with an understanding of the principles, concepts and analysis techniques of rotary-wing (RW) platforms.

This module can be taken as an Accredited Short Course or a Standalone Short Course.

Please go to the 'Upgrade to a professional qualification' section for more information.

At a glance

  • Dates
    • Please enquire for course dates
  • Duration5 days
  • LocationCranfield University at Shrivenham
  • Cost

    Accredited Short Course fee - £1,300

    Standalone Short Course fee - £1,750

    Concessions available

What you will learn

On successful completion of this module a student should be able to:

  • describe the aerodynamic principles of RW flight,
  • estimate RW component power requirements,
  • evaluate aspects of the performance of a RW platform.

Core content

Introduction:

RW a/c definitions; configurations and layout.


Rotor axial flight performance:

rotor definitions, 
thrust, induced velocity, induced power, profile and climb power in axial flight, flow states in axial flight, effects of blade geometry, rotor coefficients, disc loading and blade loading, rotor figure of merit, ground effect,vertical autorotation.

 

Rotor control:

collective and cyclic controls, 
feathering, flapping and lagging; fully-articulated, hingeless, elastomeric and bearingless rotors; teetering rotors, swash plate and spider, rotor RPM control, rotor moments.

 

Rotor forward flight:

thrust, induced velocity, induced power and profile power in forward flight, 
blade cyclic variation of speed and incidence, flap back, rotor limitations due to compressibility and stall and the effect on aircraft performance, dynamic stall effects, tip modifications, ABC, compounding, etc.

 

Rotary wing aircraft performance:

parasite power, 
minimum power and minimum drag speeds, maximum speed, range and endurance, take-off and climb, forward flight descent and autorotation, hover ceiling IGE and OGE.


RW aircraft trim, stability and control:

control at the hover and in forward flight, 
effect of rotor head design, rotor stability with respect to incidence and speed, rotor lag, a/c longitudinal, lateral and directional static and dynamic stability at the hover and in forward flight. manoeuvrability and agility.

 

Cross-couplings and vibrations:

examples of cross-coupling effects, 
ground resonance, introduction to helicopter vibration, vibration absorbers, ACSR.


Transmissions:

transmission layouts for single and multi-rotor helicopters.



Tutorials, practical demonstrations and a case study.




Upgrade to a professional qualification

When taken as an Accredited Short Course, 10 credit points can be put towards the Military Aerospace and Airworthiness MSc.

Find out more about short course credit points.

Concessions

A limited number of MOD sponsored places are available.

Location and travel

Cranfield Defence and Security (CDS) is a Cranfield University School based at the Ministry of Defence establishment at Shrivenham, on the Oxfordshire/ Wiltshire border.

Shrivenham itself lies in the picturesque Vale of the White Horse, close to the M4 motorway which links London and South Wales. It is 7 miles from Swindon, the nearest town, which lies off the M4 at the hub of Britain’s motorway network.

Bath, Cheltenham, Bristol and Oxford are all within an hour’s drive and London less than two hours away by car.

All visitors must be pre-booked in at reception by the person they are visiting on the campus.

For further location and travel details.


How to apply

To apply for this course please use the online application form.

Read our Professional development (CPD) booking conditions.