In this paper,a simplifiedtransonic weapon baywith a L/D=5 and Mach number 0.85 was considered using the large-eddy simulation(LES)with dynamic kinetic energy subgrid-scale (SGS)model.
Ali Can Fadil, Baha Zafer
doaj
A Frequency-Domain Linearized Euler Model for Noise Radiation [PDF]
Arina, Renzo +2 more
core +2 more sources
Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan. [PDF]
Ahmed F +3 more
europepmc +1 more source
Application of Swept-Sine Excitation for Acoustic Impedance Education [PDF]
The NASA Langley Normal Incidence Tube (NIT) and Grazing Flow Impedance Tube (GFIT) are regularly employed to characterize the frequency response of acoustic liners through the eduction of their specific acoustic impedance.
Howerton, Brian M. +2 more
core +1 more source
On the relevance of facesheet orifice geometry to acoustic liner impedance. [PDF]
Avallone F +5 more
europepmc +1 more source
Large-scale analysis of delayed recognition using sleeping beauty and the prince. [PDF]
Miura T, Asatani K, Sakata I.
europepmc +1 more source
Bio-Inspired Blade Cascades: Numerical Predictions Versus Experimental Measurements. [PDF]
Totu AG, Crunțeanu DE, Isvoranu D.
europepmc +1 more source
Mechanism of Pipeline Leakage Sound Generation and Leak Detection Technology Under Multiple Operational Conditions. [PDF]
Chen F +7 more
europepmc +1 more source
Validating Confined Flame Noise Simulation Using External Sensor. [PDF]
Williamson AJ, Srivastava S, Sallam KA.
europepmc +1 more source
Design and acoustic characterization of a test bench for aeroacoustic studies under controlled turbulent flow. [PDF]
Gianoli Kovar P, Cataldo Ottieri J.
europepmc +1 more source

