Contamination and Distortion of Steady Flow Field Induced by Discrete Frequency in Aircraft Gas Turbines.
Abstract
This annual technical report covers the first year, Phase I activity of a research program initiated in January 1, 1983. The main objective of the present program is to investigate the influence of Reynolds stresses of organized origin - induced by discrete frequency disturbances - in deforming and affecting the steady internal flow of aircraft engines. In particular, attention of the present research is focused upon the effect of orderly disturbances such as (A) the vortex whistle upon the Ranque-Hilsch effects and (B) Karman vortex street in causing temperature separation within the wake of bodies.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 16, 1984
- Accession Number
- ADA147092
Entities
People
- M. Kurosaka
Organizations
- University of Tennessee Space Institute