Nothing Special   »   [go: up one dir, main page]

Chen et al., 2018 - Google Patents

High-temperature effects on aerodynamic and acoustic characteristics of a rectangular supersonic jet

Chen et al., 2018

View PDF
Document ID
6250347040725435367
Author
Chen S
Gojon R
Mihaescu M
Publication year
Publication venue
2018 AIAA/CEAS aeroacoustics conference

External Links

Snippet

Implicit large-eddy simulations (LES) are performed in this work to study the flow field and acoustic characteristics of a rectangular supersonic jet. The focus is to investigate the high- temperature effects, ie when the jet total temperature is as high as 2100 K. Four cases with a …
Continue reading at hal.science (PDF) (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation

Similar Documents

Publication Publication Date Title
Chen et al. High-temperature effects on aerodynamic and acoustic characteristics of a rectangular supersonic jet
Kovasznay Turbulence in supersonic flow
Yoder et al. Modeling of turbulent free shear flows
Nichols et al. Crackle noise in heated supersonic jets
Prasad et al. A study of noise reduction mechanisms of jets with fluid inserts
Li et al. Acoustic feedback loops for screech tones of underexpanded free round jets at different modes
Barone et al. Receptivity of the compressible mixing layer
Prasad et al. Effect of fluid injection on turbulence and noise reduction of a supersonic jet
Chen et al. Flow and aeroacoustic attributes of highly-heated transitional rectangular supersonic jets
Bodony et al. Jet noise prediction of cold and hot subsonic jets using large-eddy simulation
Chen et al. Nozzle pressure ratio effects on aerodynamics and acoustics of a highly-heated rectangular supersonic jet
Arroyo et al. Azimuthal mode analysis of broadband shock-associated noise in an under-expanded axisymmetric jet
Birkby et al. Numerical predictions of turbulent underexpanded sonic jets using a pressure-based methodology
Sousa et al. Nonlinear Spectral Broadening Dynamics of Second Mode Waves on a Hypersonic Flared Cone
Wu et al. Three-dimensional numerical study of the acoustic properties of a highly underexpanded jet
Li et al. The source localization and dynamical evolution of axisymmetric screech modes in underexpanded supersonic jets
Ahn et al. Flow and near-field pressure fluctuations of twin square jets
Frendi et al. Flow structures and noise from a supersonic impinging jet
Johnson et al. Flow and noise characteristics of under-and over-expanded supersonic rectangular jets
Prasad et al. Assessment of a generalized acoustic variable for supersonic jet noise
Jain et al. Sound generation in multicomponent nozzle flows with dissipation
Khobragade et al. Linear and nonlinear flow analysis of elements of a supersonic inlet
Ji et al. Numerical investigation of acoustically excited flow through an orifice using lattice Boltzmann method
Lui et al. A numerical investigation of broad-band shock noise
Cuppoletti et al. Analysis of supersonic jet thrust with fluidic injection