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SEDL / STP / STP68-EB
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STP68
Symposium on Materials for Gas Turbines
Committee A01
Pages: 204
Published: 1946
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Table of Contents
Introduction
Mochel N.
Joint Discussion
Heat-Resisting Metals for Gas-Turbine Parts
Cross H., Simmons W.
High-Temperature Alloys Developed for Aircraft Turbosuperchargers and Gas Turbines
Freeman J., Reynolds E., White A.
Chromium-Base Alloys
Parke R., Bens F.
Metallurgy of High-Temperature Alloys Used on Current Gas Turbine Designs
Badger F., Sweeny W.
Alloys and Ceramic Materials for High-Temperature Service
Cross H.
Resistance of Iron-Nickel-Chromium Alloys to Corrosion in Air at 1600 to 2200 F
Brasunas A., Gow J., Harder O.
Compressive Properties of Aluminum Alloy Sheet at Elevated Temperatures
Flanigan A., Tedsen L., Dorn J.
Tensile and Creep Strengths of Some Magnesium-Base Alloys at Elevated Temperature
Moore A., McDonald J.
Committee: A01
Paper ID: STP68-EB
DOI: 10.1520/STP68-EB
ISBN-EB: 978-0-8031-5905-1
 ASTM International is a member of CrossRef.
0-8031-6059-3
978-0-8031-6059-0
STP68-EB
STP 68
STP 680
STP 681
STP 682
STP 683
STP 684
STP 685
STP 686
STP 687
STP 688
STP 689
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