Published online by Cambridge University Press: 26 October 2023
Considerable work has been done on wind tunnel testing of helicopter and autogyro rotors and of specific helicopter fuselages but there is no available information on the wind tunnel development of a complete design prior to construction of a prototype helicopter With interest in the stability and control of helicopters and to assist the development of a specific design the wind tunnel development was undertaken by the Aeronautical Research Laboratories
Acknowledgement is made to the Chief Scientist, Department of Supply, Australia, for permission to publish this paper