Numerical Propagation of Aircraft En-route Noise
Author | : Kieran Poulain |
Publisher | : |
Total Pages | : 260 |
Release | : 2011 |
Genre | : |
ISBN | : |
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Author | : Kieran Poulain |
Publisher | : |
Total Pages | : 260 |
Release | : 2011 |
Genre | : |
ISBN | : |
Author | : Oleksandr Zaporozhets |
Publisher | : CRC Press |
Total Pages | : 432 |
Release | : 2011-05-13 |
Genre | : Technology & Engineering |
ISBN | : 0203888820 |
Aircraft noise has adverse impacts on passengers, airport staff and people living near airports, it thus limits the capacity of regional and international airports throughout the world. Reducing perceived noise of aircraft involves reduction of noise at source, along the propagation path and at the receiver. Effective noise control demands highly s
Author | : A-21 Aircraft Noise Measurement Aviation Emission Modeling |
Publisher | : |
Total Pages | : 0 |
Release | : 2020 |
Genre | : |
ISBN | : |
This document describes methods for calculating the attenuation of sound due to line-of-sight blockage or shielding from non-level terrain. This method applies to sound propagating from an airplane to locations on the ground during ground roll, climbout after liftoff, and landing operations.AIR1845 and AIR5662 provides guidance for modeling aircraft noise at airports with flat terrain. In reality, many airports are surrounded by non-level terrain that may result in attenuation (or shielding) of sound at some receptors. This noise blockage can be accounted for with the line-of-sight blockage calculation, based on the difference in propagation path length between the direct path and propagation path over the top of terrain feature. The purpose of this aircraft information report is to provide a method that accounts for the attenuation due to line-of-sight blockage of aircraft noise by terrain features. This Aerospace Information Report (AIR) describes a method to calculate noise level adjustments due to line-of-sight blockage (LOS) of the noise propagation between a source and receiver by terrain for the purposes of aircraft noise prediction modeling.AIR1845 provides guidance for modeling aircraft noise at airports with flat terrain. In reality, many airports are surrounded by non-level terrain that may result in noise blockage (or shielding) at some nearby receptors. This noise blockage can be accounted for with the line-of-sight blockage calculation, based on the difference in propagation path length between the direct path (straight line between source and receiver, terrain feature absent) and the propagation path over or around the terrain feature.
Author | : Erik Petersen |
Publisher | : |
Total Pages | : |
Release | : 2015 |
Genre | : |
ISBN | : |
Predictions of absorption and dispersion of en-route aircraft noise in the atmosphere are produced using the ANSI S1.26 [1] algorithm and an updated algorithm by Sutherland and Bass [2].Disagreement between predicted absorption coefficients are attributed to differences between the two models and reference atmospheric profiles, with the latter responsible for more variation than the former. In particular, the molar concentration of H2O is found to be a significant factor for absorption predictions in the atmosphere. Using the Sutherland and Bass algorithm, the relative contribution of separate physical absorption mechanisms, including classical thermoviscous effects, rotational relaxation, and vibrational relaxation losses, are compared as a function of frequency and altitude. It is found that vibrational relaxation is the dominant loss mechanism over the frequency range of 125 to 1000 Hz at altitudes of 0 to 10 km. Although vibrational relaxation gives way to classical losses above 10 km, it is shown that carbon dioxide-induced vibrational relaxation contributes up to 14% of the total losses at 15 km altitude. To evaluate the impact of absorption coefficients for a propagating wave, cumulative absorption over a vertical propagation path can be calculated by numerical integration. It is shown that the discretization step sizes should be no greater than 1 km to avoid under sampling the absorption curves from 0 to 18 km altitude. Finally, dispersion is analyzed by calculating the phase speed increment due to O2, N2, CO2, and O3 as a function of altitude. Dispersion due to O2 accounts for approximately 85% of the phase speed increment from 0 to 18 km. At 0 km, the N2-induced phase speed increment accounts for the majority of the remaining 15%, but decreases with increasing altitude. The percent contribution of CO2 is small at 0 km, and increases to 14% at 18 km. The CO2-induced dispersion, not typically included in sound propagation models, may effect sonic boom shock structure of supersonic aircraft at cruise altitudes.
Author | : Great Britain. Noise Advisory Council |
Publisher | : |
Total Pages | : 46 |
Release | : 1974 |
Genre | : Air traffic control |
ISBN | : |
Author | : Lothar Bertsch |
Publisher | : Mdpi AG |
Total Pages | : 0 |
Release | : 2022-08-15 |
Genre | : Technology & Engineering |
ISBN | : 9783036548982 |
Noise generated by aircraft continues to be a pressing issue for society, as an increasing number of people residing in close proximity to airports make noise complaints on a regular basis. The reduction in aircraft noise is therefore a very important engineering task that would require the careful identification of different acoustic sources around the airplane, the understanding of noise source behavior and ranking along flight trajectories, sophisticated measurement techniques, and robust and accurate numerical tools aimed at predicting the generation of noise, the propagation through the atmosphere, and the resulting noise impact along approach and departure flights. For an overall assessment of the situation, it has to be assessed along entire flight trajectories rather than assessing limited operating conditions only. Furthermore, it is highly recommended to apply multiple acoustic metrics and account for different and widespread observer locations along the flight. Only then can the overall situation be adequately captured. Obviously, this is a highly multidisciplinary effort and no single discipline can address this problem. This reprint includes selected research studies with that multidisciplinary context that deal with numerical or experimental investigations that range from the investigation of specific noise sources to the assessment of noise generated by the overall aircraft in operation. Both basic and applied research studies involving the modelling and simulation of aircraft noise are included.
Author | : |
Publisher | : |
Total Pages | : 704 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Author | : G. J. J. Ruijgrok |
Publisher | : IOS Press |
Total Pages | : 360 |
Release | : 2004 |
Genre | : Science |
ISBN | : |
"The purpose of this book is to provide insight into those elements of acoustics and aeronautics that are connected directly with the problem of aviation noise. It is intended as a textbook for a university course on aviation acoustics at an undergraduate level. The simplicity of presentation also lends itself to the book's use as an instrument of selfstudy for the practicing engineer. The contents of the book are a reflection of an annual course on aviation noise presented by the author to senior undergraduate students of aerospace engineering at Delft University of Technology."--BOOK JACKET.
Author | : William James Hadden |
Publisher | : |
Total Pages | : |
Release | : 1974 |
Genre | : Airplanes |
ISBN | : |
Author | : Donald P. Garber |
Publisher | : |
Total Pages | : 36 |
Release | : 1994 |
Genre | : Airplanes |
ISBN | : |