Direct numerical simulation of transition and turbulence in a spatially evolving boundary layerA high-order-accurate finite-difference approach to direct simulations of transition and turbulence in compressible flows is described. Attention is given to the high-free-stream disturbance case in which transition to turbulence occurs close to the leading edge. In effect, computation requirements are reduced. A method for numerically generating free-stream disturbances is presented.
Document ID
19910056156
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rai, Man M. (NASA Ames Research Center Moffett Field, CA, United States)
Moin, Parviz (NASA Ames Research Center Moffett Field; Stanford University, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-1607Report Number: AIAA PAPER 91-1607