Actions for Computed Temperature Distribution and Cooling of Solid Gas-Turbine Blades

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Computed Temperature Distribution and Cooling of Solid Gas-Turbine Blades

Author
Gazley, Carl, Jr.
Published
February 11, 1947.
Physical Description
1 electronic document
Additional Creators
Reuter, J. George
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Computations were made to determine the temperature distribution and cooling of solid gas-turbine blades.A range of temperatures was used from 1500 degrees to 2500 degrees F, blade-root temperatures from 100 degrees to 1000 degrees F, blade thermal conductivity from 8 to 220 BTU/(hr)(sq ft)(degrees F/ft), and net gas to metal heat transfer coefficients from 75 to 250 BTU/(hr)(sq ft)(degrees F).
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20030064303.
NACA-RM-E7B11h.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15636635