Author: Douglas Aircraft Company
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 178
Book Description
The effects of compressive loads on structural fatigue at elevated temperatures are investigated using plain, notched, and welded Titanium 8Al-1Mo-1V, and PH 15-7Mo stainless steel coupon specimens. Specimens are subjected to Mach 3 spectrum test environment, including compressive loads. Fatigue life predictions are compared with spectrum teset results. The influence of prior stress-strain history on subsequent life is considered. Prediction methods are extended to include the compression range, and results notched specimens is determined analytically and experimentally. A variety of individual variable fatigue tests are performed at temperatures up to 900F.
Effect of Compressive Loads on Structural Fatigue at Elevated Temperature
Author: Douglas Aircraft Company
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 178
Book Description
The effects of compressive loads on structural fatigue at elevated temperatures are investigated using plain, notched, and welded Titanium 8Al-1Mo-1V, and PH 15-7Mo stainless steel coupon specimens. Specimens are subjected to Mach 3 spectrum test environment, including compressive loads. Fatigue life predictions are compared with spectrum teset results. The influence of prior stress-strain history on subsequent life is considered. Prediction methods are extended to include the compression range, and results notched specimens is determined analytically and experimentally. A variety of individual variable fatigue tests are performed at temperatures up to 900F.
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 178
Book Description
The effects of compressive loads on structural fatigue at elevated temperatures are investigated using plain, notched, and welded Titanium 8Al-1Mo-1V, and PH 15-7Mo stainless steel coupon specimens. Specimens are subjected to Mach 3 spectrum test environment, including compressive loads. Fatigue life predictions are compared with spectrum teset results. The influence of prior stress-strain history on subsequent life is considered. Prediction methods are extended to include the compression range, and results notched specimens is determined analytically and experimentally. A variety of individual variable fatigue tests are performed at temperatures up to 900F.
Scientific and Technical Aerospace Reports
U.S. Government Research Reports
Metallic Materials and Elements for Flight Vehicle Structures
Author:
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 790
Book Description
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 790
Book Description
Monthly Catalog of United States Government Publications
Metallic Materials and Elements for Aerospace Vehicle Structures
Author: United States. Department of Defense
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 820
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 820
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
Book Description
Composite Structures for Civil and Architectural Engineering
Author: D-H Kim
Publisher: CRC Press
ISBN: 9780419191704
Category : Architecture
Languages : en
Pages : 522
Book Description
A thorough and understandable guide to the properties and design of structural composites. It derives from the author's many years of experience of research, industrial development and teaching.
Publisher: CRC Press
ISBN: 9780419191704
Category : Architecture
Languages : en
Pages : 522
Book Description
A thorough and understandable guide to the properties and design of structural composites. It derives from the author's many years of experience of research, industrial development and teaching.