Simulation of shock / boundary layer interactions using improved LES/RANS models

Daniel A. Gieseking, Jung Il Choi, Jack R. Edwards, Hassan A. Hassan

Research output: Chapter in Book/Report/Conference proceedingConference contribution

11 Citations (Scopus)

Abstract

A new hybrid large-eddy simulation / Reynolds-averaged Navier-Stokes simulation (LES/RANS) method is presented in this work. In this approach, the resolved turbulence kinetic energy, ensemble-averaged modeled turbulence kinetic energy and turbulence frequency, and time-resolved turbulence frequency are used to form an estimate of an outer-layer length scale that is nearly Reynolds-number independent. The ratio of this outer-layer scale with an inner-layer length scale (proportional to the wall distance) is used to construct a blending function that facilitates the shift between an unsteady RANS formulation near solid surfaces and an LES formulation away from the wall. The new model is tested through simulations of compressible flat-plate boundary layers over a wide range of Reynolds numbers and Mach 2.85 flow over a smooth compression ramp. The results show that the new model provides results for mean and second-moment statistics that are in good agreement with experiment and are comparable to those obtained using the original model (Edwards, et al., AIAA J., 2008), which required a case-by-case calibration of a model constant.

Original languageEnglish
Title of host publication48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Publication statusPublished - 2010 Dec 13
Event48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: 2010 Jan 42010 Jan 7

Other

Other48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
CountryUnited States
CityOrlando, FL
Period10/1/410/1/7

Fingerprint

Large eddy simulation
Boundary layers
Turbulence
Kinetic energy
Reynolds number
Mach number
Statistics
Calibration
Experiments

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Gieseking, D. A., Choi, J. I., Edwards, J. R., & Hassan, H. A. (2010). Simulation of shock / boundary layer interactions using improved LES/RANS models. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition [2010-0111]
Gieseking, Daniel A. ; Choi, Jung Il ; Edwards, Jack R. ; Hassan, Hassan A. / Simulation of shock / boundary layer interactions using improved LES/RANS models. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010.
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Gieseking, DA, Choi, JI, Edwards, JR & Hassan, HA 2010, Simulation of shock / boundary layer interactions using improved LES/RANS models. in 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition., 2010-0111, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, United States, 10/1/4.

Simulation of shock / boundary layer interactions using improved LES/RANS models. / Gieseking, Daniel A.; Choi, Jung Il; Edwards, Jack R.; Hassan, Hassan A.

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-0111.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Gieseking DA, Choi JI, Edwards JR, Hassan HA. Simulation of shock / boundary layer interactions using improved LES/RANS models. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-0111