Prediction of Aeroacoustic and Control over a Cavity by Delayed Detached Eddy Simulation

Yu Liu; Ming Bo Tong

doi:10.4028/www.scientific.net/AMM.598.505

Paper Titles

Research on Recommendation System Selection Based on Fuzzy VIKOR with Multiple Distances
p.481

Eigenfunctions of Rayleigh Wave in Viscoelastic Halfspace
p.486

Backward Difference Scheme for Simulating Unsteady Compressible Flow on Deforming Mesh in an Implicit Adaptive Solver
p.493

Semi-Forward Adaptive Simulation Approach for Tube Hydroforming Loading Path Determination Using a Strain Trajectory Based Fuzzy Logic Control
p.498

Prediction of Aeroacoustic and Control over a Cavity by Delayed Detached Eddy Simulation
p.505

Control of FES-Assisted Elliptical Stepping Exercise Using Fuzzy Logic Controller
p.510

Implementation of PID Controller with PSO Tuning for FES-Assisted Exercise
p.516

Modeling and Controller Comparison for Quarter Car Suspension System by Using PID and Type-1 Fuzzy Logic
p.524

Theoretical Investigation of a Structure for Active Vibration Control with Fuzzy Logic Approach
p.529

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 598Prediction of Aeroacoustic and Control over a...

Prediction of Aeroacoustic and Control over a Cavity by Delayed Detached Eddy Simulation

Abstract:

In the present study CFD simulation with delayed detached eddy simulation (DDES) are performed to investigate an open cavity at Mach 0.85. Two cavity configurations, clean cavity and cavity with a leading-edge saw tooth spoiler, are modeled. The results obtained from clean cavity prediction are compared with experimental sound pressure level (SPL) data from QinetiQ, UK. Furthermore, comparisons are made with the predicted SPL between the two configurations. The main focuses of this investigation are to obtain a further understanding of the cavity aeroacoustics and test the noise suppression effect by a saw tooth spoiler.

You might also be interested in these eBooks

Advanced Materials, Mechanics and Industrial Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 598)

Pages:

505-509

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.598.505

Citation:

Cite this paper

Online since:

July 2014

Authors:

Yu Liu*, Ming Bo Tong

Keywords:

Aeroacoustic, Cavity, Delayed Detached Eddy Simulation, Spalart-Allmaras, Spoiler

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Mark H. Morton, Craig D. Hampson, Ric A. Alexander: Final Vibration and Acoustic Loads Development for Certification of the F-22 Advanced Tactical Fighter. In: 49th AIAA / ASME / ASCE / AHS / ASC Structures, Structural Dynamics, and Materials Conference, Schaumburg, IL, USA (2008).

DOI: 10.2514/6.2008-1901

Google Scholar

[2] Smagorinsky. J.: General Circulation Experiments with the Primitive Equations. Monthly Weather Review, 91 (1963).

DOI: 10.1175/1520-0493(1963)091<0099:gcewtp>2.3.co;2

Google Scholar

[3] G.W. Foster, J.A. Ross, and R.M. Ashworth: Weapon Bay Aerodynamics-Wind-Tunnel Trials and CFD Modelling by QinetiQ UK. In: RTO/AVT Symposium on Flow-Induced Unsteady Loads and the Impact on Military Applications, Budapest, Hungary (2005).

Google Scholar

[4] Henshaw, M.J. de C.: M219 cavity case. In: Verification and Validation Data for Computational Unsteady Aerodynamics, Tech. Rep. RTO-TR-26, AC/323 (AVT) TP/19, QinetiQ, UK (2000).

Google Scholar

[5] Shoeb Ahmed Syed, Klaus A. Hoffmann: Numerical Investigation of 3-D Open Cavity with and Without Cover Plates. In: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, USA (2009).

DOI: 10.2514/6.2009-551

Google Scholar

[6] Punit Nayyar, in: CFD Analysis of Transonic Turbulent Cavity Flows, chapter 7, submitted to the Faculty of Engineering, University of Glasgow (2005).

Google Scholar

[7] Xiaoxian Chen, Neil D. Sandham and Xin Zhang: Cavity Flow Noise Predictions. Final Report for MSTARR DARP (2007).

Google Scholar