GAS-TURBINE ROTOR TEMPERATURE FIELD WITH COOLING AIR BLOWN THROUGH SLOTS IN ROOT ATTACHMENTS,
Abstract
Topics include: rotor temperature field, effect of cooling-airflow rate and leakage into the flow-through section of the rotor temperature field, effective coolingair temperature on rotor temperature field, and some rotor temperature-field considerations with cooling air supplied to ring seals and to disk faces.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 21, 1965
- Accession Number
- AD0627113
Entities
People
- K. P. Seleznev
Organizations
- National Air and Space Intelligence Center