Hostname: page-component-cd9895bd7-fscjk Total loading time: 0 Render date: 2024-12-28T22:35:39.831Z Has data issue: false hasContentIssue false

The design and Development of the Helicopter Rotor Testing Tower

Published online by Cambridge University Press:  28 July 2016

Extract

From the start of the development of helicopters at the Bristol Aeroplane Company the necessity was appreciated of providing means of testing, independently of the aircraft, rotor hubs and blades. The usual method of testing on the helicopter suffers from several disadvantages, the most important being that proximity of the ground beneath the rotor greatly affects the flow through it and makes such performance figures as can be obtained unrepresentative. Others are the probable inconvenience of having to wait for the completion of the aircraft before rotor-testing can start, the comparative difficulty of instrumentation, and the risk of damage to the aircraft by failure or misbehaviour of the rotor.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1949

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)