Accession Number:

AD0627113

Title:

GAS-TURBINE ROTOR TEMPERATURE FIELD WITH COOLING AIR BLOWN THROUGH SLOTS IN ROOT ATTACHMENTS,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1965-12-21

Pagination or Media Count:

19.0

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.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE