Flow Field Diagnostics in the Compressor Research Facility One-Tenth Scale Flow Model.
Abstract
The Air Force Aero Propulsion Laboratory is developing a compressor research facility (CRF). The facility must provide a metered flow at a given pressure which is uniform in temperature and velocity at the compressor inlet. In this study the flow field of a one-tenth scale flow model of the CRF, constructed by a contractor for the Air Force Aero Propulsion Laboratory, was investigated. Velocity measurements made with a constant temperature anemometer using hot wire sensors provided the basis for establishing velocity profiles and turbulence intensity levels.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1975
- Accession Number
- ADA023360
Entities
People
- Tsuyoshi Shinji
Organizations
- Air Force Institute of Technology