High-Temperature Alloys Developed for Aircraft Turbosuperchargers and Gas Turbines

J. Freeman; E. Reynolds; A. White

doi:10.1520/STP44967S

SYMPOSIA PAPER Published: 01 January 1946

STP44967S

High-Temperature Alloys Developed for Aircraft Turbosuperchargers and Gas Turbines

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In recognition of the advantages to be obtained through the use of the gas turbine in aircraft power plants, the National Advisory Committee for Aeronautics started to sponsor research work in November, 1941, to develop suitable heat-resistant alloys. This paper describes the alloys which have evolved from the phase of their work conducted under contracts at the University of Michigan. Due to necessary restrictions under wartime conditions, the results have previously only been given limited circulation.

Author Information

Freeman, J., W.

University of Michigan, Ann Arbor, Mich.

Reynolds, E., E.

University of Michigan, Ann Arbor, Mich.

White, A., E.

University of Michigan, Ann Arbor, Mich.

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Details

Developed by Committee: A01

Pages: 52–79

DOI: 10.1520/STP44967S

ISBN-EB: 978-0-8031-5905-1

ISBN-13: 978-0-8031-6059-0

High-Temperature Alloys Developed for Aircraft Turbosuperchargers and Gas Turbines

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