Results 21 to 30 of about 304 (177)
Comparative study of surface integral methods in aeroacoustic prediction
Introduction: Surface integral methods based on the acoustic analogy and Kirchhoff formulation are widely employed in computational aeroacoustics. The computational accuracy is usually highly dependent on the selections of the acoustic prediction method ...
Chen Xu +5 more
doaj +1 more source
Progress and prospective of computational aeroacoustics [PDF]
The origin and research category of Computational Aeroacoustics (CAA) are introduced firstly. The early progress and applications are summarized, focusing on the two key elements of CAA, high accuracy spatial and time discretization schemes and non-reflecting boundary conditions.
DaKai LIN +5 more
openaire +1 more source
Experimental and Computational Aeroacoustic Investigation of Small Rotor Interactions in Hover
This paper investigates the aeroacoustic interactions of small hovering rotors, using both experiments and computations. The experiments were conducted in an anechoic chamber with arrays of microphones setup to evaluate the azimuthal and polar ...
Austin David Thai +6 more
doaj +1 more source
A numerical investigation using 3D RANS simulations demonstrates significant effects of protuberance geometry—cubic, cylindrical, spherical, and conical—on shock‐induced thrust vectoring in supersonic nozzles. Cubic protuberances provide the maximum jet deflection (˜2°) with negligible thrust reduction.
Mohammadreza Soufivand +3 more
wiley +1 more source
We present the extension of a discontinuous Galerkin framework to zonal direct-hybrid aeroacoustic simulations. This extension provides the ability to simultaneously perform a zonal large eddy simulation (LES), solving the compressible Navier–Stokes ...
Kempf Daniel, Munz Claus-Dieter
doaj +1 more source
This research explores how fluid flow, structural movement, and sound interact in an elastic baffle system. Using a numerical approach based on the finite element method, the study analyzes how noise and vibrations change with different baffle configurations. The findings reveal that shortening the baffle by half reduces noise transmission by 9%, while
Tohid Adibi +5 more
wiley +1 more source
The present paper is aimed at providing an updated review of prediction methods for the aerodynamic noise of ducted rotor–stator stages. Indeed, ducted rotating-blade technologies are in continuous evolution and are increasingly used for aeronautical ...
Stéphane Moreau, Michel Roger
doaj +1 more source
Aerospace Engineering Undergraduate Laboratory Courses: A Systematic Review (1990–2025)
ABSTRACT This review examines the evolution of undergraduate aerospace engineering (AE) laboratories from 1990 to 2025, focusing on course formats, pedagogy, technology, and assessment. Once centered on traditional demonstration‐based exercises, AE laboratories have increasingly shifted toward hands‐on, project‐based, and hybrid physical‐virtual models
Mingtai Chen
wiley +1 more source
Computational Aeroacoustics Analysis and the Impact of Acoustic Materials on Aircraft Noise Reduction [PDF]
As the aviation industry continues to pursue sustainable, eco-friendly solutions, aeroacoustic analysis has become essential for achieving noise-reduction objectives.
Phillip Christina +2 more
doaj +1 more source
Quantum algorithms for differential equations are developed with applications in computational fluid dynamics. The methods follow an iterative simulation framework, implementing Jacobi and Gauss–Seidel schemes on quantum registers through linear combinations of unitaries.
Chelsea A. Williams +4 more
wiley +1 more source

