THE PREDICTION OF AIRFRAME NOISE AND COMPARISON WITH EXPERIMENT
โ Scribed by G.M. LILLEY
- Book ID
- 102607498
- Publisher
- Elsevier Science
- Year
- 2001
- Tongue
- English
- Weight
- 175 KB
- Volume
- 239
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
โฆ Synopsis
The success of the high bypass ratio turbofan engine in reducing the external noise of civil transport aircraft at take-o! and landing, while improving the economics of air travel, has opened up the debate as to how much further it will be possible to reduce aircraft noise by the introduction of new aircraft or existing aircraft retro"tted with new engines. Irrespective of what new technology can o!er in respect of further engine noise reduction for no loss of performance, it is now clear that all future aircraft will require airframe noise to be reduced on the approach, since today it is comparable with engine noise. This paper discusses the major components of airframe noise and reviews the present state of airframe noise prediction. Finally, a comparison is made between prediction and experimental data and the prospects for airframe noise reduction.
2001 Academic Press
๐ SIMILAR VOLUMES
Accurate prediction of ''buzz-saw'' noise in a turbofan inlet duct necessitates consideration of nonlinear acoustics, modelling a complete fan blade set, modelling an acoustic liner, and calculations at high frequencies. A recent series of papers has described new work concerning the application of
A center-cracked pa&l of 707Saluminum alloy which has over-aged from the T651 condition was loaded in tension and subsequently unloaded to zero applied load. The permanent surface deformation was measured close to the intersections of the crack front with the free surfaces. The permanent deformation