Accession Number : AD0616713

Title :   THE EFFECT OF SOUND WAVES AND FLEXIBLE BOUNDARIES OF TURBULENCE.

Descriptive Note : Master's thesis,

Corporate Author : OKLAHOMA UNIV NORMAN

Personal Author(s) : Fisher,Donald Herbert

Report Date : 1965

Pagination or Media Count : 46

Abstract : Research was conducted on separation of boundary layers on airfoils at high angles of attack, and skin friction drag in laminar and turbulent boundary layers on airfoils at low angles of attack. (Author)

Descriptors :   *AIRFOILS, *BOUNDARY LAYER, *SOUND, *TURBULENCE, *TURBULENT BOUNDARY LAYER, ANEMOMETERS, DAMPING, DRAG, LAMINAR FLOW, LIFT, SEPARATION, SOUND, TURBULENCE, WAKE, WINGS

Distribution Statement : APPROVED FOR PUBLIC RELEASE