Recent Australian full-scale F/A-18 fatigue tests (2009)
Barter, S.A., Molent, L., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programmes in support of the through-life structural integrity of the Royal Australian Air Force (RAAF) F/A-18...
Recent Australian full-scale F/A-18 fatigue tests (2009)
Barter, S.A., Molent, L., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programmes in support of the through-life structural integrity of the Royal Australian Air Force (RAAF) F/A-18...
Recent Australian full-scale F/A-18 fatigue tests (2009)
Barter, S.A., Molent, L., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programmes in support of the through-life structural integrity of the Royal Australian Air Force (RAAF) F/A-18...
Recent Australian full-scale F/A-18 fatigue tests (2009)
Barter, S.A., Molent, L., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programmes in support of the through-life structural integrity of the Royal Australian Air Force (RAAF) F/A-18...
Damage tolerance demonstration testing for the Australian F/A-18 (2008)
Molent, L., Barter, S.A., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programs in support of the through-life structural integrity of the Royal Australian Air Force’s (RAAF)...
Damage tolerance demonstration testing for the Australian F/A-18 (2008)
Molent, L., Barter, S.A., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programs in support of the through-life structural integrity of the Royal Australian Air Force’s (RAAF)...
Damage tolerance demonstration testing for the Australian F/A-18 (2008)
Molent, L., Barter, S.A., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programs in support of the through-life structural integrity of the Royal Australian Air Force’s (RAAF)...
Damage tolerance demonstration testing for the Australian F/A-18 (2008)
Molent, L., Barter, S.A., White, P., Dixon, B.
Over recent years Australia has been involved in a number of full-scale fatigue testing programs in support of the through-life structural integrity of the Royal Australian Air Force’s (RAAF)...
Liu, Q., Yang, C.H., Ding, K., Barter, S.A., Ye, L.
Laser shock peening (LSP) is an innovative surface treatment method that can result in significant improvement in the fatigue life of many metallic components. The process produces very little or no...
Liu, Q., Yang, C.H., Ding, K., Barter, S.A., Ye, L.
Laser shock peening (LSP) is an innovative surface treatment method that can result in significant improvement in the fatigue life of many metallic components. The process produces very little or no...
Liu, Q., Yang, C.H., Ding, K., Barter, S.A., Ye, L.
Laser shock peening (LSP) is an innovative surface treatment method that can result in significant improvement in the fatigue life of many metallic components. The process produces very little or no...
Liu, Q., Yang, C.H., Ding, K., Barter, S.A., Ye, L.
Laser shock peening (LSP) is an innovative surface treatment method that can result in significant improvement in the fatigue life of many metallic components. The process produces very little or no...
Liu, Q., Ding, K., Ye, L., Rey, C., Barter, S. A., Sharp, P. K., ...
Laser shock peening (LSP) is a promising surface treatment for fatigue life extension of metallic materials. The benefits include deeper residual stresses (>1 mm) and a smoother surface finish than...
The Effectiveness Of Repairing Fatigue Damaged 7050 Aluminium Alloy Using Shot Peening (2004)
Liu, Q., Hu, W., Barter, S. A., Sharp, P. K.
Shot peening is an effective life extension surface treatment process. In this study, experiments were performed to investigate whether shot peening could be used to recover the fatigue resistance of...
The Effectiveness Of Repairing Fatigue Damaged 7050 Aluminium Alloy Using Shot Peening (2004)
Liu, Q., Hu, W., Barter, S. A., Sharp, P. K., Atrens, A., Boland, J. N., ...
Shot peening is an effective life extension surface treatment process. In this study, experiments were performed to investigate whether shot peening could be used to recover the fatigue resistance of...
Liu, Q., Ding, K., Ye, L., Rey, C., Barter, S. A., Sharp, P. K., ...
Laser shock peening (LSP) is a promising surface treatment for fatigue life extension of metallic materials. The benefits include deeper residual stresses (>1 mm) and a smoother surface finish than...
Liu, Q., Ding, K., Ye, L., Rey, C., Barter, S. A., Sharp, P. K., ...
Laser shock peening (LSP) is a promising surface treatment for fatigue life extension of metallic materials. The benefits include deeper residual stresses (>1 mm) and a smoother surface finish than...
The Effectiveness Of Repairing Fatigue Damaged 7050 Aluminium Alloy Using Shot Peening (2004)
Liu, Q., Hu, W., Barter, S. A., Sharp, P. K.
Shot peening is an effective life extension surface treatment process. In this study, experiments were performed to investigate whether shot peening could be used to recover the fatigue resistance of...
Liu, Q., Ding, K., Ye, L., Rey, C., Barter, S. A., Sharp, P. K., ...
Laser shock peening (LSP) is a promising surface treatment for fatigue life extension of metallic materials. The benefits include deeper residual stresses (>1 mm) and a smoother surface finish than...
The Effectiveness Of Repairing Fatigue Damaged 7050 Aluminium Alloy Using Shot Peening (2004)
Liu, Q., Hu, W., Barter, S. A., Sharp, P. K.
Shot peening is an effective life extension surface treatment process. In this study, experiments were performed to investigate whether shot peening could be used to recover the fatigue resistance of...
DSTO research into material factors likely to affect F/A-18 fatigue life has highlighted a number of concerns about the fatigue variability of the 7050 thick section plate and the effect that the...
DSTO research into material factors likely to affect F/A-18 fatigue life has highlighted a number of concerns about the fatigue variability of the 7050 thick section plate and the effect that the...
AVD research into material factors likely to affect F/A-18 fatigue life has highlighted the critical role played by surface condition in determining the service fatigue life of aircraft structure....
AVD research into material factors likely to affect F/A-18 fatigue life has highlighted the critical role played by surface condition in determining the service fatigue life of aircraft structure....
This report presents the results of a fatigue coupon test program. The primary purpose was to obtain results from coupons with a surface condition typical of some Ion Vapour Deposited Aluminium alloy...
This report presents the results of a fatigue coupon test program. The primary purpose was to obtain results from coupons with a surface condition typical of some Ion Vapour Deposited Aluminium alloy...
A closure model to crack growth under large-scale yielding and through residual stress fields (2003)
Wang, C.H., Barter, S.A., Liu, Q.
This paper presents a closure model for predicting the growth behavior of short cracks in the presence of large-scale yielding and residual compressive stresses, representative of structures that...
DSTO research into material factors likely to affect F/A-18 fatigue life has highlighted a number of concerns about the fatigue variability of the 7050 thick section plate and the effect that the...
This report presents the results of a fatigue coupon test program. The primary purpose was to obtain results from coupons with a surface condition typical of some Ion Vapour Deposited Aluminium alloy...
AVD research into material factors likely to affect F/A-18 fatigue life has highlighted the critical role played by surface condition in determining the service fatigue life of aircraft structure....
A closure model to crack growth under large-scale yielding and through residual stress fields (2003)
Wang, C.H., Barter, S.A., Liu, Q.
This paper presents a closure model for predicting the growth behavior of short cracks in the presence of large-scale yielding and residual compressive stresses, representative of structures that...
U) 4. AUTHOR(S) 5. CORPORATE AUTHOR 506 Lorimer St Fishermans Bend Victoria 3207 Australia 6a. DSTO NUMBER 6b. AR NUMBER 6c. TYPE OF REPORT Technical Report 7. DOCUMENT DATE 8. FILE NUMBER...
DSTO research into material factors likely to affect F/A-18 fatigue life has highlighted a number of concerns about the fatigue variability of the 7050 thick section plate and the effect that the...
This report presents the results of a fatigue coupon test program. The primary purpose was to obtain results from coupons with a surface condition typical of some Ion Vapour Deposited Aluminium alloy...
AVD research into material factors likely to affect F/A-18 fatigue life has highlighted the critical role played by surface condition in determining the service fatigue life of aircraft structure....
A closure model to crack growth under large-scale yielding and through residual stress fields (2003)
Wang, C.H., Barter, S.A., Liu, Q.
This paper presents a closure model for predicting the growth behavior of short cracks in the presence of large-scale yielding and residual compressive stresses, representative of structures that...
A closure model to crack growth under large-scale yielding and through residual stress fields (2003)
Wang, C.H., Barter, S.A., Liu, Q.
This paper presents a closure model for predicting the growth behavior of short cracks in the presence of large-scale yielding and residual compressive stresses, representative of structures that...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
On August 20, 1998 a United States Marine Corps F/A-18 aircraft crashed at RAAF Delamere bombing range in the Northern Territory. AMRL was invited to aid in the investigation by trialing AMRL Global...
On August 20, 1998 a United States Marine Corps F/A-18 aircraft crashed at RAAF Delamere bombing range in the Northern Territory. AMRL was invited to aid in the investigation by trialing AMRL Global...
During the investigation of aircraft accidents and incidents, it is usually a requirement that the wreckage parts, ground marks and other interesting features at the incident site are identified and...
During the investigation of aircraft accidents and incidents, it is usually a requirement that the wreckage parts, ground marks and other interesting features at the incident site are identified and...
On August 20, 1998 a United States Marine Corps F/A-18 aircraft crashed at RAAF Delamere bombing range in the Northern Territory. AMRL was invited to aid in the investigation by trialing AMRL Global...
During the investigation of aircraft accidents and incidents, it is usually a requirement that the wreckage parts, ground marks and other interesting features at the incident site are identified and...
On August 20, 1998 a United States Marine Corps F/A-18 aircraft crashed at RAAF Delamere bombing range in the Northern Territory. AMRL was invited to aid in the investigation by trialing AMRL Global...
During the investigation of aircraft accidents and incidents, it is usually a requirement that the wreckage parts, ground marks and other interesting features at the incident site are identified and...
RAAF Orion Aircraft A9-300 Oxygen Fire, (1998)
This report summarizes the findings of the investigation into the nature and cause of the fire in RAAF Orion aircraft A9-300. This aircraft was destroyed by fire which initiated in the oxygen system...
Examination of the Microstructure of 7050 Aluminum Alloy Samples. (1998)
Barter, S. A., Athiniotis, N., Lambrianidis, L.
As part of the evaluation of the structural life of the F/A-18 fighter aircraft, samples of the Aluminum Alloy 7050 taken from several different fatigue specimens, including F/A-18 FS 488 Bulkhead...
Fractographic inspection of the cracking FT488/2 removed at program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead FatigueTest specimen after 79 blocks of applied loading, cracking was found in several wing-attachment hole aft edges. Each of the cracked regions...
Fractographic inspection of the cracking FT488/2 removed at program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead FatigueTest specimen after 79 blocks of applied loading, cracking was found in several wing-attachment hole aft edges. Each of the cracked regions...
Fractographic inspection of the cracking FT488/2 removed at program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead FatigueTest specimen after 79 blocks of applied loading, cracking was found in several wing-attachment hole aft edges. Each of the cracked regions...
Fractographic Inspection of the Cracking FT488/2 Removed at Program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead Fatigue Test specimen after 79 blocks of applied loading, the starboard upper wing-attachment hole aft edge, port lower wing-attachment hole aft...
Fractographic inspection of the cracking FT488/2 removed at program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead FatigueTest specimen after 79 blocks of applied loading, cracking was found in several wing-attachment hole aft edges. Each of the cracked regions...
Fractographic inspection of the cracking FT488/2 removed at program 79 (1998)
During the inspection of the FT488/2 Bare Bulkhead FatigueTest specimen after 79 blocks of applied loading, cracking was found in several wing-attachment hole aft edges. Each of the cracked regions...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...