Hostname: page-component-586b7cd67f-r5fsc Total loading time: 0 Render date: 2024-11-25T02:55:18.906Z Has data issue: false hasContentIssue false

Canadian Research in the Field of Helicopter Icing

Published online by Cambridge University Press:  26 October 2023

J R Stallabrass*
Affiliation:
National Research Council, Ottawa

Extract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

The CHAIRMAN, in opening the meeting, said that the paper, which Mr Stallabrass had come over from Canada to present, dealt with a very important subject in the helicopter field, having as a practical objective the eventual achievement of all-weather helicopter operation The National Research Council of Canada had been studying the problem of aircraft icing long before it was necessary to devote attention to the special problems of helicopter de-icing, no doubt the climate in that part of the world having had something to do with this

Mr Stallabrass had served in the Royal Air Force from 1941 to 1947 and had experience as a pilot with Coastal Command in anti-submarine operations Later, he took an honours degree at London University in electrical engineering and worked for a year on guided missiles with the General Electric Company In 1952 he went over to Canada, where he worked on various aspects of icing research at the low temperature laboratory of the National Research Council

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1958

References

1 Messinger, B L Equilibrium Temperature of an Unheated Icing Surface as a Function of Airspeed Journal of Aeronautical Sciences, Vol 20, p 29, January, 1953CrossRefGoogle Scholar
2 Rush, C K, and Wardlaw, R L Wind Tunnel Simulation of Atmospheric Icing Conditions National Aeronautical Establishment paper presented to AGARD 5th General Assembly, Ottawa, June, 1955Google Scholar
3 Robertson, E O Preliminary Helicopter Icing Flight Trials National Aeronautical Establishment Lab Rept LR-106 July, 1954Google Scholar
4 Bailey, D L Description of the Spray Rig Used to Study Icing on Helicopters in Flight National Aeronautical Establishment Lab Rept LR-186 January, 1957Google Scholar
5 Stallabrass, J R Helicopter Icing Research National Research Council Quarterly Bulletin, April-June, 1957Google Scholar
6 Stallabrass, J R Some Aspects of Helicopter Icing Canadian Aeronautical Journal, Vol 3, No 8, October, 1957Google Scholar
7 Richardson, D A, Wahl, H A, and Clifford, J M Solutions for Helicopter Rotor Blade Icing Presented to 26th annual meeting of Institute of Aeronautical Sciences, January 27—30, 1958 (Preprint 810)Google Scholar
8 Fraser, D The Characteristics of an Orifice-type Icing-detector Probe National Aeronautical Establishment Lab Rept LR-71 June, 1953Google Scholar
9 Dickey, T A An Analysis of the Effects of Certain Variables in Determining the Form of an Ice Accretion U S Navy, Naval Air Material Center, AEL-1206, 1952Google Scholar
10 Langmuir, I, and Blodgett, K B A Mathematical Investigation of Water Droplet Trajectories U S AAF Tech Rept 5418, February, 1946Google Scholar