An Investigation of Scale-Resolving Turbulence Models for Supersonic Retropropulsion Flows
Characterization of unsteady loads is critical for the development of control systems for next-generation air vehicles. Both Direct Numerical Simulation (DNS) and Large Eddy Simulation (LES) methods are prohibitively expensive, and existing Reynolds-Averaged Navier-Stokes (RANS) approaches have been...
Main Authors: | Gabriel Nastac, Abdelkader Frendi |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-11-01
|
Series: | Fluids |
Subjects: | |
Online Access: | https://www.mdpi.com/2311-5521/7/12/362 |
Similar Items
-
Analysis of Propellant Weight under Re-Entry Conditions for a Reusable Launch Vehicle Using Retropropulsion
by: Yongchan Kim, et al.
Published: (2021-05-01) -
Improved Supersonic Turbulent Flow Characteristics Using Non-Linear Eddy Viscosity Relation in RANS and HPC-Enabled LES
by: Kalyani Bhide, et al.
Published: (2021-11-01) -
APPLICABILITY OF VARIOUS DIFFERENTIAL TURBULENCE MODELS IN THE CALCULATION OF SUPERSONIC GAS JETS
by: E. E. Il'ina, et al.
Published: (2015-05-01) -
Verification of calculated characteristics of supersonic turbulent jets
by: Julia V. Fisher, et al.
Published: (2017-02-01) -
Study of Transition to Turbulence in a Supersonic Boundary Layer Using DNS and Transition Prediction
by: Hiroshi MAEKAWA
Published: (2007-12-01)