Forward acoustic performance of a shock-swallowing high-tip-speed fan (QF-13) [PDF]
Forward noise and overall aerodynamic performance data are presented for a high-tip-speed fan having rotor blade airfoils designed to alter the conventional leading-edge bow shocks to weak, oblique shocks which are swallowed within the interblade ...
Lucas, J. G. +2 more
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Jet noise suppression by porous plug nozzles [PDF]
Jet noise suppression data presented earlier by Maestrello for porous plug nozzles were supplemented by the testing of a family of nozzles having an equivalent throat diameter of 11.77 cm.
Bauer, A. B., Kibens, V., Wlezien, R. W.
core +1 more source
Vehicle Aerodynamic Noise: A Systematic Review of Mechanisms, Simulation Methods, and Bio-Inspired Mitigation Strategies. [PDF]
Zou T, Fu Y, Cao P.
europepmc +1 more source
Metasurface Lossless-Regulation Mechanism of Dynamic Acoustic Mass for Low-Frequency Aerodynamic Noise Control. [PDF]
Li M, Wu J.
europepmc +1 more source
Bio-inspired helical pantograph arms for aerodynamic noise suppression in high-speed trains. [PDF]
Lou F, Xiao X, Zhang Z, Zhang J, Li X.
europepmc +1 more source
Interim noise correlation for some OTW configurations using external jet-flow deflectors [PDF]
Jet flap interaction acoustic data obtained statically from a model-scale study of STOL-OTW configurations with a conical nozzle mounted above the wing and using various external deflectors to provide jet-flow attachment are correlated. The acoustic data
Groesbeck, D. E., Vonglahn, U. H.
core +1 more source
Owl airfoil aerodynamic noise sources and performance compared to hawk and NACA0012 airfoils for low Reynolds applications. [PDF]
Kazemi M, Mani M.
europepmc +1 more source
Analytical Solution and Analysis of Aerodynamic Noise Induced by the Turbulent Flow Interaction of a Plate with Double-Wavelength Bionic Serration Leading Edges. [PDF]
Tian C, Liu X, Wang L, Li Y, Wu Y.
europepmc +1 more source
Aerodynamic and acoustic performance of ejectors for engine-under-the-wing concepts [PDF]
Subsonic thrust augmentation, exhaust plume velocity contours and acoustic characteristics of a small-scale, 6-tube mixer nozzle with ejector were obtained with and without a wing. Thrust augmentation up to 30 percent was achieved.
Goodykoontz, J. H. +2 more
core +1 more source
Aerodynamic noise characteristics of a centrifugal fan in high-altitude environments. [PDF]
Liu X, Liu J.
europepmc +1 more source

