Explore Books on
turbulent boundary layer

A near-wall Reynolds-stress closure without wall normals

By S. P. Yuan

EPOCS-1981 summary data report

By H. P. Hanson

Turbulent-flow separation criteria for overexpanded supersonic nozzles

By E. Leon Morrisette

Transitional boundary-layer solutions using a mixing-length and a two-equation turbulence model

By E. Clay Anderson

Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations

By Neal T. Frink

Three-dimensional turbulent-mixing-length modeling for discrete-hole coolant injection into a crossflow

By Chi R. Wang

Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3

By M. I. Kussoy

A k-[epsilson] modeling of near wall turbulence

By Z. Yang

Hypersonic shock/boundary-layer interaction database

By Gary S. Settles

Roughness-induced generation of crossflow vortices in three-dimensional boundary layers

By Meelan Choudhari

Implementation of a two-equation K-[omega] turbulence model in NPARC

By Dennis A. Yoder

Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9

By William D. Deveikis

Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3

By J. E. Bardina

In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0

By Robert D. Quinn

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63-012 airfoil

By James C. Yu

Turbulente Scherströmungen

By Witold Szablewski

Near-wall, three-dimensional turbulence measurements

By D. A. Johnson

Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3

By Seymour M. Bogdonoff

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation

By Richard W. Barnwell

Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

By Sheryll Goecke Powers

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

By David S. Dolling

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8

By L. Roane Hunt

Simulation of boundary-layer transition

By Fabio P. Bertolotti

Simple turbulence models and their application to boundary layer separation

By Alan Wadcock