On the differences in noise predictions based on solid and permeable surface Ffowcs Williams–Hawkings integral solutions
Author:
Affiliation:
1. Boeing Commercial Airplanes, Seattle, USA
2. Peter the Great St Petersburg Polytechnic University, St Petersburg, Russia
3. New Technologies and Services (NTS), St Petersburg, Russia
Publisher
SAGE Publications
Subject
Acoustics and Ultrasonics,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/1475472X19878934
Reference22 articles.
1. On the precise implications of acoustic analogies for aerodynamic noise at low Mach numbers
2. The influence of solid boundaries upon aerodynamic sound
3. Sound generation by turbulence and surfaces in arbitrary motion
4. Initial noise predictions for rudimentary landing gear
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