This paper serves as part I of a two-part tutorial on “aero-optical effects.” We first present background information to assist with our introduction of the topic. Next, we use the …
J Panda - Journal of Fluid Mechanics, 1999 - cambridge.org
The screech noise generation process from supersonic underexpanded jets, issuing from a sonic nozzle at pressure ratios of 2.4 and 3.3 (fully expanded Mach number, Mj= 1.19 and …
This paper gives the most-complete characterization to date of the optical aberrations imposed on a laser beam propagated through a subsonic, compressible, turbulent boundary …
K Wang, M Wang - Journal of Fluid Mechanics, 2012 - cambridge.org
Compressible large-eddy simulations are carried out to study the aero-optical distortions caused by Mach 0.5 flat-plate turbulent boundary layers at Reynolds numbers of, 1770 and …
A Mani, P Moin, M Wang - Journal of fluid mechanics, 2009 - cambridge.org
The flow over a circular cylinder at ReD= 3900 and 10000 and M= 0.4 is considered a platform to study the aero-optical distortions by separated shear layers and turbulent wakes …
Wall-modeled large-eddy simulations of turbulent boundary-layer flows over a flat plate at Mach 3.5, 7.87, and 13.64 were carried out, and the aero-optical distortions resulting from …
J Cao, P Wang, Y Liu - Physics of Fluids, 2024 - pubs.aip.org
Incompressible large eddy simulations of dual purging jets at three Reynolds numbers of Re L= 1500, 1000, and 500 are performed, providing the database for simulated interferometric …
This paper serves as part II of a two-part tutorial on “aero-optical effects.” In part I, we provide introductory material with an emphasis on system-level considerations, particularly for those …
A Mani, M Wang, P Moin - Journal of Computational Physics, 2008 - Elsevier
Analytical criteria are developed to estimate the error of aero-optical computations due to inadequate spatial resolution of refractive index fields in high Reynolds number flow …