Hostname: page-component-76fb5796d-22dnz Total loading time: 0 Render date: 2024-04-29T23:38:11.779Z Has data issue: false hasContentIssue false

Towards a silent aircraft

Published online by Cambridge University Press:  03 February 2016

A.P. Dowling
Affiliation:
Department of Engineering, University of Cambridge, Cambridge, UK
T. Hynes
Affiliation:
Department of Engineering, University of Cambridge, Cambridge, UK

Abstract

We set a target for a ‘Silent’ aircraft to be imperceptible outside the airfield perimeter in an urban environment, and then address conceptual designs to meet this requirement. Avoiding some traditional aircraft noise sources requires a radical rethink about the configuration. An all-lifting design has many benefits, enabling a closer integration of airframe and engine than the traditional ‘tube and wing’. Low-noise design includes taking advantage of shielding of engine noise by the airframe; low-noise engines with large, low speed jets; an order of magnitude increase in absorption by liners; and operations for low-noise informing the design. Progress to date on the Silent Aircraft Initiative is presented, along with some conceptual aircraft and engine designs. The further work needed to develop these into viable future aircraft is discussed.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 2006 

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.)

References

1. ACARE, European Aeronautics: A Vision for 2020, Advisory Council for Aeronautics Research in Europe, 2000.Google Scholar
2. Wakayama, S., Blended-wing-body optimization problem set-up, 2000, AIAA Paper 2000-4740.Google Scholar
3. Lighthill, M.J., On sound generated aerodynamically, Part I: General Theory, Proc Roy Soc A, 1952, 211, pp 564587.Google Scholar
4. Crichton, D., Xu, L. and Hall, C.A., Preliminary fan design for a silent aircraft, 2006, ASME2006-90564.Google Scholar
5. Liebeck, R.H., Design of the blended wing body subsonic commercial transport, AIAA J Aircr, 2004, 41, pp 1025.Google Scholar
6. Hileman, J.I., Spakovszky, Z.S., Drela, M. and Sargeant, M.A., Aerodynamic and aeroacoustic three-dimensional design for a ‘silent’ aircraft, 2006, AIAA 2006-241.Google Scholar
7. Crichton, D. and Hall, C.A., Engine and installation configurations for a silent aircraft, 2005 ISABE-2005-1164.Google Scholar
8. Hall, C.A. and Crichton, D., Engine design studies for a silent aircraft, 2006 ASME- GT2006-90559.Google Scholar
9. Agarwal, A. and Dowling, A.P., Low-frequency acoustic shielding by the silent aircraft airframe, 2005, AIAA-2005-2996.Google Scholar
10. Agarwal, A., Dowling, A.P., Shin, H., Graham, W. and Sefi, S., Acoustic shielding by the silent aircraft airframe, 2006, AIAA-2006-2618.Google Scholar
11. Law, T.R. and Dowling, A.P., Optimization of traditional and blown liners for a silent aircraft, 2006, AIAA-2006-2525.Google Scholar
12. SAI engine team, private communication.Google Scholar
13. Shin, H., Graham, W. and Sijtsma, P., Design and implementation of a phased microphone array in a closed-section wind tunnel, 2006, AIAA-2006-2651.Google Scholar
14. Andreou, C., Graham, W. and Shin, H., Aeroacoustic study of airfoil leading edge high-lift devices, 2006, AIAA-2006-2515.Google Scholar
15. SAI team, private communication.Google Scholar