Axial-load Fatigue Tests on Notched Sheet Specimens of 24S-T3 and 75S-T6 Aluminum Alloys and of SAE 4130 Steel with Stress-concentration Factors of 2.0 and 4.0 PDF Download
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Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
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Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
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Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
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Book Description
Author: Harold N. Cummings
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 596
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 518
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1304
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Book Description
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
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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: Rudolph Earl Peterson
Publisher: Wiley-Interscience
ISBN:
Category : Science
Languages : en
Pages : 342
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Book Description
Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
Author: John S. Evans
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 668
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Book Description
Because the chemical reaction rates needed to predict the dependence of degree of dissociation on distance behind the shock are not known, order-of-magnitude estimates of their values have been used in a numerical example, the purpose of which is to illustrate the use of reaction-rate equations to predict relaxation time and distance behind the shock front.
