TY - GEN
T1 - Wave Packet Development in Three-Dimensional Low-Speed Laminar Boundary Layers
AU - Bahrainirad, Ladan
AU - Hosseinverdi, Shirzad
AU - Fasel, Hermann F.
N1 - Funding Information:
This work was supported by the Army Research Office (ARO) under grant number W911NF1910100, with Dr. Matthew Munson serving as the program manager. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the Army Research Office or the U. S. Government. Computer time for numerical simulations was provided by the University of Arizona High Performance Computing center.
Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2021
Y1 - 2021
N2 - Direct numerical simulations are employed to investigate ‘natural’ laminar-turbulent transition in three-dimensional incompressible boundary layers with favorable-pressure gradients. Toward this end, the evolution of three-dimensional wave packets in swept laminar boundary layers is investigated, where the wave packets are generated by a localized short-duration pulse disturbance. First, the weakly nonlinear development of a wave packet in a two-dimensional zero-pressure gradient boundary-layer, guided by the wind-tunnel experiments of Gaster & Grant (1975), served as a validation for a Navier-Stokes solver based on a disturbance flow formulation that was developed in our laboratory. Next, the development of a wave packet in a three-dimensional boundary-layer initiated by a small amplitude pulse was examined. It was found that both stationary and traveling crossflow modes were generated with wide range of spanwise wavenumbers, with traveling modes reaching the largest maximum amplitude. By increasing the pulse forcing amplitude, the nonlinear evolution of the wave packet was investigated. Fourier decomposition clearly indicates a cascade of nonlinearly generated higher harmonics of the primary unsteady crossflow disturbances. Nonlinear mechanisms eventually trigger the transition process and the final breakdown to turbulence.
AB - Direct numerical simulations are employed to investigate ‘natural’ laminar-turbulent transition in three-dimensional incompressible boundary layers with favorable-pressure gradients. Toward this end, the evolution of three-dimensional wave packets in swept laminar boundary layers is investigated, where the wave packets are generated by a localized short-duration pulse disturbance. First, the weakly nonlinear development of a wave packet in a two-dimensional zero-pressure gradient boundary-layer, guided by the wind-tunnel experiments of Gaster & Grant (1975), served as a validation for a Navier-Stokes solver based on a disturbance flow formulation that was developed in our laboratory. Next, the development of a wave packet in a three-dimensional boundary-layer initiated by a small amplitude pulse was examined. It was found that both stationary and traveling crossflow modes were generated with wide range of spanwise wavenumbers, with traveling modes reaching the largest maximum amplitude. By increasing the pulse forcing amplitude, the nonlinear evolution of the wave packet was investigated. Fourier decomposition clearly indicates a cascade of nonlinearly generated higher harmonics of the primary unsteady crossflow disturbances. Nonlinear mechanisms eventually trigger the transition process and the final breakdown to turbulence.
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U2 - 10.2514/6.2021-2897
DO - 10.2514/6.2021-2897
M3 - Conference contribution
AN - SCOPUS:85126790265
SN - 9781624106101
T3 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021
BT - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021
Y2 - 2 August 2021 through 6 August 2021
ER -