Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 0

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An investigation was conducted to determine the low-cycle (under 10 000 cycles) crack growth characteristics of through- center- cracked specimens 0.060 in. (0.152 cm) thick subjected to tension-tension cyclic loading. The following factors were studied: (1) minimum to maximum initial stress intensity ratio R (sub i); (2) the maximum gross stress applied, as percentage of critical fracture stress; and (3) cyclic rate. The crack growth rate was found to be a function of stress level expressed as percentage of critical fracture stress for specimens tested at the same R. value. A crack growth relation was developed which takes into account changes in R. in the low-cycle region. When the cycle rate was decreased from 0. 5 to 0.05 Ha, the cyclic life was reduced, but only for high initial stress intensities.

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 0

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Book Description
An investigation was conducted to determine the low-cycle (under 10 000 cycles) crack growth characteristics of through- center- cracked specimens 0.060 in. (0.152 cm) thick subjected to tension-tension cyclic loading. The following factors were studied: (1) minimum to maximum initial stress intensity ratio R (sub i); (2) the maximum gross stress applied, as percentage of critical fracture stress; and (3) cyclic rate. The crack growth rate was found to be a function of stress level expressed as percentage of critical fracture stress for specimens tested at the same R. value. A crack growth relation was developed which takes into account changes in R. in the low-cycle region. When the cycle rate was decreased from 0. 5 to 0.05 Ha, the cyclic life was reduced, but only for high initial stress intensities.

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -3200 F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -3200 F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 52

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Factors Influencing Low-Cycle Crack Growth in 2014-T6 Aluminum Sheet at -320 F (77 K).

Factors Influencing Low-Cycle Crack Growth in 2014-T6 Aluminum Sheet at -320 F (77 K). PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 45

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Book Description
An investigation was conducted to determine the low-cycle (under 10 000 cycles) crack growth characteristics of through- center- cracked specimens 0.060 in. (0.152 cm) thick subjected to tension-tension cyclic loading. The following factors were studied: (1) minimum to maximum initial stress intensity ratio R (sub i); (2) the maximum gross stress applied, as percentage of critical fracture stress; and (3) cyclic rate. The crack growth rate was found to be a function of stress level expressed as percentage of critical fracture stress for specimens tested at the same R. value. A crack growth relation was developed which takes into account changes in R. in the low-cycle region. When the cycle rate was decreased from 0. 5 to 0.05 Ha, the cyclic life was reduced, but only for high initial stress intensities.

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category :
Languages : en
Pages : 41

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NASA Technical Note

NASA Technical Note PDF Author:
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Category :
Languages : en
Pages : 430

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NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
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Category : Aeronautics
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Category : Government publications
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NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Category : Science
Languages : en
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A Selected Listing of NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Category : Aeronautics
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Pages : 962

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