The Unsteady Flow Physics and Aeroacoustics Laboratory of Stanford University works in association with the Department of Aeronautics and Astronautics and with the Flow Physics and Compuation Division of the Mechanical Engineering Department.

The research areas of current focus include turbulence simulations, compressible shear flows, transition in boundary layers, aeroacoustics, jet noise, turbine blade heat transfer, aircraft vortex wakes and condensation trails, and numerical methods. Computational techniques are developed and used to study the fluid dynamics of a variety of problems.

This site is to serve as a platform for information exchange. Research within the laboratory is conducted open to peer review. When appropriate, papers, figures, movies, and data will be available, provided proper credit is given to the original author(s). Questions regarding this policy should be directed to Prof. Lele.