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Problems in the Application of High-Strength Steel Alloys in the Design of SUPERSONIC Aircraft

Published 1958-01-01 by SAE International in United States
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Lightweight Springs for Limited Life

Published 1956-01-01 by SAE International in United States
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Fatigue and Fail-Safe Airframe Design

Published 1956-01-01 by SAE International in United States
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The Selection of Metals for Airframe Components as Affected by Operation at Elevated Temperatures up to 600 F

Published 1956-01-01 by SAE International in United States
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PRACTICAL APPLICATION OF STRESS STRAIN THEORY IN FABRICATION OF AIRCRAFT PARTS

Published 1943-01-01 by SAE International in United States
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preliminary design considerations for the Structure of a Trisonic Transport

Published 1960-01-01 by SAE International in United States
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THE FIRST CONSTELLATION DECADE

Published 1955-01-01 by SAE International in United States
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Flight Load Measurements and Analysis

Published 1955-01-01 by SAE International in United States
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Strength and Thermal Limitations of Materials for Airframe Components

Published 1959-01-01 by SAE International in United States
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status of the SAE S-12 approach to VIBRATION ISOLATION of Aircraft Electronic Equipment

Published 1959-01-01 by SAE International in United States
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