Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
Book Description
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
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
Book Description
Axial-load Fatigue Tests on Edge-notched Sheet Specimens of 2024-T3 and 7075-T6 Aluminum Alloys and of SAE 4130 Steel with Notch RadII of 0.004 and 0.070 Inch
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Axial-load Fatigue Tests on Notched Sheet Specimens of 24S-T3 and 75S-T6 Aluminum Alloys and of SAE 4130 Steel with Stress-concentration Factor of 1.5
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
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 5.0
Author: H. J. Grover
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Some Quantitative Aspects of Fatigue of Materials
Author: Harold N. Cummings
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 596
Book Description
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 596
Book Description
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 518
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 518
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1304
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1304
Book Description
Fatigue Strengths of Aircraft Materials
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
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.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
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.
Stress Concentration Factors
Author: Rudolph Earl Peterson
Publisher: Wiley-Interscience
ISBN:
Category : Science
Languages : en
Pages : 342
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.
Publisher: Wiley-Interscience
ISBN:
Category : Science
Languages : en
Pages : 342
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.
Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves
Author: John S. Evans
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 668
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.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 668
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.