Exploratory investigation of combustion and NVH signature of a drone jet engine fueled with IPK
V Soloiu, CJ Phillips, C Carapia, A Knowles… - AIAA Scitech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1347. vid The pollution from
aerospace transportation is rapidly becoming the largest source of greenhouse gas (GHG) …
aerospace transportation is rapidly becoming the largest source of greenhouse gas (GHG) …
Computational study of the effect of structural compliance on the noise radiated from an elastic trailing-edge
M Nardini, RD Sandberg, SC Schlanderer - Journal of Sound and Vibration, 2020 - Elsevier
The effect of the structural compliance of an elastic trailing-edge (TE) on its aeroacoustic
response is investigated by means of Direct Numerical Simulation. For that purpose, a two …
response is investigated by means of Direct Numerical Simulation. For that purpose, a two …
Using acoustic liner for fan noise reduction in modern turbofan engines
With the increase in global air travel, aircraft noise has become a major public issue. In
modern aircraft engines, only a small proportion of the air that passes through the whole …
modern aircraft engines, only a small proportion of the air that passes through the whole …
Direct Numerical Simulation of the Acoustic Response of a NACA-0012 Airfoil with an Elastic Serrated Trailing-Edge
M Nardini, RD Sandberg - 30th AIAA/CEAS Aeroacoustics Conference …, 2024 - arc.aiaa.org
Direct Numerical Simulation (DNS) is adopted to investigate the acoustic response of a
NACA-0012 airfoil with an elastic serrated trailing-edge (TE) extension. To study the airfoil …
NACA-0012 airfoil with an elastic serrated trailing-edge (TE) extension. To study the airfoil …
Main fan noise mitigation technologies in turbofan engines
Aircraft noise and emissions have been of concern since the beginning of commercial
aviation. The continuing growth in air traffic and increasing public awareness have made …
aviation. The continuing growth in air traffic and increasing public awareness have made …
Experimental validation of a shape-memory alloy slat-cove filler: Structural response and computational model development
R Patterson, W Scholten, T Strganac… - Journal of Intelligent …, 2020 - journals.sagepub.com
Current and expected Federal Aviation Administration regulations are pressuring the
aerospace industry to develop new technologies that reduce aeroacoustic emissions, which …
aerospace industry to develop new technologies that reduce aeroacoustic emissions, which …
Low-frequency interior noise in prop-driven aircrafts: Sources and control methodologies
Nowadays, noise has turned into one of the most important among the environmental factors
on which industry sets down a big part of its efforts and concerns. The recognition of noise …
on which industry sets down a big part of its efforts and concerns. The recognition of noise …
[PDF][PDF] Supersonic Jet Noise: Main Sources and Reduction Methodologies.
The large velocity ratio and the presence of Shocks in the exhaust plume from low bypass
engines or supersonic jetliners cause jet noise to be dominant component of overall aircraft …
engines or supersonic jetliners cause jet noise to be dominant component of overall aircraft …
An investigative study of combustion and emissions with noise and vibrations of synthetic fuels within an aero-gas turbine
CJ Phillips - 2020 - digitalcommons.georgiasouthern …
The pollution from the aerospace transportation is rapidly becoming the largest source of
greenhouse gas (GHG) emissions. The FAA expects aviation emissions to almost triple by …
greenhouse gas (GHG) emissions. The FAA expects aviation emissions to almost triple by …
Reduced-order modeling and acoustic optimization of the noise generated by boundary layer instabilities convecting over an elastic trailing-edge
M Nardini, RD Sandberg - Aiaa Aviation 2020 Forum, 2020 - arc.aiaa.org
A novel reduced-order fluid-structure interaction acoustic model for the noise generated by
the unsteady deflection of an elastic trailing-edge (TE) subjected to an incident pressure …
the unsteady deflection of an elastic trailing-edge (TE) subjected to an incident pressure …