Fatigue Strengths of Aircraft Materials PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Fatigue Strengths of Aircraft Materials PDF full book. Access full book title Fatigue Strengths of Aircraft Materials by Horace John Grover. Download full books in PDF and EPUB format.
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
Get Book Here
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
Get Book Here
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.
Author: Horace John Grover
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 22
Get Book Here
Book Description
Results are given of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and of normalized SAE 4130 steel. Each specimen was notched by edge notches designed to have a theoretical stress-concentration factor of 1.5. Tests were run at nominal mean stresses of 0, 10,000, 20,000, and 30,000 psi. Results extend previously reported data on unnotched specimens and specimens more severly notched data on the variation of fatigue strength with notch severity.
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Get Book Here
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel. Each specimen was notched by edge notches designed to have a theoretical stress-concentration factor of 5.0. Tests were run at nominal mean stresses of 0, 10,000, 20,000, and 30,000 psi. Results extend previously reported data on unnotched specimens and specimens less severely notched.
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 25
Get Book Here
Book Description
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 0
Get Book Here
Book Description
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Get Book Here
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel. Each specimen was notched by edge notches designed to have a theoretical stress-concentration factor of 5.0. Tests were run at nominal mean stresses of 0, 10,000, 20,000, and 30,000 psi. Results extend previously reported data on unnotched specimens and specimens less severely notched.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Get Book Here
Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Get Book Here
Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Get Book Here
Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
Get Book Here
Book Description
