The objective of this investigation is to study the velocity-field sources
for the fluctuating wall pressure, determine their locations in the boundar
y layer, and investigate their physics. The velocity-field sources and part
ial wall pressures were computed from a database generated by a direct nume
rical simulation of a low Reynolds number, fully developed, turbulent chann
el flow. Results show that the mean-shear (MS) and turbulence-turbulence (T
T) partial pressures (pi(MS) and pi(TT), respectively) are the same order o
f magnitude. The buffer region dominates most of the wave number range; the
viscous shear layer is significant at the highest wavenumbers; the buffer
and logarithmic regions are important at low wavenumbers. Over most of the
wavenumber range, the contribution from the buffer region is the dominant T
T component; in the low-wavenumber range, the viscous shear layer, buffer r
egion, and logarithmic region are significant; in the medium and high waven
umbers the viscous shear layer and buffer region dominate. The most importa
nt TT partial pressures are pi(23)(TT), pi(13)(TT) and pi(12)(TT) from the
buffer region. It is conjectured that pi(23)(TT) and pi(13)(TT) may be gene
rated by quasi-streamwise vortices. pi(12)(TT) may be due to near-wall shea
r layers and spanwise vortices. pi(23)(TT), pi(22)(TT) and pi(33)(TT) from
the viscous shear layer are the dominant high-wavenumber partial pressures.
(C) 1999 American Institute of Physics. [S1070-6631(99)02511-8].