Almost 40 Years of Airframe Noise Research: What Did We Achieve?

作者: Werner Dobrzynski

DOI: 10.2514/1.44457

关键词:

摘要: IN THE early 1970s the first twin cycle bypass turbofan engines came into service. The development of such engines was triggered by the need to reduce fuel consumption but also had a beneficial side effect on aircraft noise impact through the corresponding reduction in jet noise. In the last decades the bypass ratio of the following generations of turbofan engines was continuously increased. As a result, aircraft engine noise now has come down to a level comparable to that of noise originating from the turbulent flow around the airframe …

参考文章(67)
M. Goodwin, M. Pott-Pollenske, D. Foot, W. Dobrzynski, Landing gears aerodynamic interaction noise ,(2004)
M. FINK, D. BAILEY, Model tests of airframe noise reduction concepts American Institute of Aeronautics and Astronautics Conference. ,(1980) , 10.2514/6.1980-979
Nicolas Molin, Jean-Francois Piet, Leung Choi Chow, Malcolm Smith, Werner Dobrzynski, Christelle Seror, Prediction of low noise aircraft landing gears and comparison with test results aiaa ceas aeroacoustics conference. ,(2006) , 10.2514/6.2006-2623
Werner Dobrzynski, Leung Chow, Pierre Guion, Derek Shiells, Research into Landing Gear Airframe Noise Reduction aiaa ceas aeroacoustics conference. ,(2002) , 10.2514/6.2002-2409
David Lockard, Mehdi Khorrami, Fei Li, Aeroacoustic Analysis of a Simplified Landing Gear aiaa ceas aeroacoustics conference. ,(2003) , 10.2514/6.2003-3111
Casey L. Burley, Thomas F. Brooks, William M. Humphreys, John W. Rawls, ANOPP Landing-Gear Noise Prediction with Comparison to Model-Scale Data aiaa ceas aeroacoustics conference. ,vol. 8, pp. 445- 475 ,(2007) , 10.1260/147547209788549299