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The High Speed Track Facility and its Comparison with other Full Scale Testing Techniques

Published online by Cambridge University Press:  04 July 2016

D. Howe
D. Howe*
Affiliation:
Cranfield Institute of Technology
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Extract

In the fourteenth Henson and Stringfellow lecture delivered to the Society earlier this year, Speechley compared the development of the helicopter with that of conventional fixed-wing aircraft. He pointed out that some ten years elapsed between Kittyhawk and the mass production of military aircraft which occurred during the First World War, and that there were a further two decades before the commercial breakthrough of the DC2/3 aircraft. Initial helicopter progress followed a similar pattern but the commercial breakthrough is still awaited more than twenty years after the beginning of large-scale military procurement.

Type
Test Facilities for Helicopters
Information
The Aeronautical Journal , Volume 74 , Issue 716 , August 1970 , pp. 643 - 649
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

1. Speechley, J. A Review of Engineering Developments in Helicopter Design. The Aeronautical Journal of the Royal Aeronautical Society Vol 73, No 705, September 1969.Google Scholar
2. Fozard, J. W. The Harrier—An Engineering Commentary. The Aeronautical Journalof theRoyal Aeronautical Society, Vol 73, No 705, September 1969.Google Scholar
3. Kirk, J. A. Experience with a V/STOL Wind Tunnel. The Journal of the Royal Aeronautical Society, Vol 71, No 681, September 1967.Google Scholar
4. Brown, D. W. An evaluation of the first series of flapping experiments with a see-saw rotor up to μ = 0·5 in open air conditions usinga vehicle for translational speed. (Unpublished RAE Technical Report) May 1967.Google Scholar
5. Smith, M. C. G. The Use of a Runway Vehicle for Testing Lifting Rotors in Simulated Forward Flight. Aeronautical Journal of the Royal Aeronautical Society, Vol. 74, No 715, July 1970.Google Scholar
6. ISELY. High speed test tracks City and Suburban Travel. Journal of Transit Research Foundation of Los Angeles, 1960.Google Scholar
7. Curtis, H. C, Putman, W. F., Traybar, J. J. The Princetown dynamic model track. AIAA Aerodynamic Testing Conference pp 33-41, March 1964.Google Scholar
8. V/STOL Track Test Facility. The Institute of Space and Aeronautical Science, University of Tokyo, ISAS Report 437. 1969.Google Scholar
9. Walker, G. E. Mobile Aerodynamic Test Facility, West- land Helicopters Ltd. Research Proposal. (Unpublished) November 1968.Google Scholar