DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click HERE
to register or log in.
Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers
Final rept. Sep 1974-Jan 1975
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Pagination or Media Count:
This report describes the results of analytical, numerical, and experimental investigations of incompressible and compressible boundary layers. The subjects considered are 1 Laminar andor turbulent numerical boundary-layer calculations in which the Reynolds stress is related to the turbulent kinetic energy 2 an analytical investigation of turbulence near a wall which is not founded on classical mixing-length theory 3 analytical solutions for relating velocity and temperature throughout turbulent boundary layers for nonunity Prandtl numbers 4 a description of the data reduction of pitot pressure measurements utilizing these analytical results, and 5 the application of the numerical and analytical results to the analysis of turbulent boundary-layer measurements made in the Propulsion Wind Tunnel Facility PWT.
APPROVED FOR PUBLIC RELEASE