-
1
-
-
34547520988
-
-
Boeing.com/commercial/Aeromagazine, Issue 24_Quarter 04, 2006.
-
Boeing.com/commercial/Aeromagazine, Issue 24_Quarter 04, 2006.
-
-
-
-
2
-
-
0034431838
-
Smith Industries HUMS: Changing the M from Monitoring to Management
-
Larder, B., Azzam, H., Trammel, C., Vossler, G., Smith Industries HUMS: Changing the M from Monitoring to Management, Proceedings of the IEEE Aerospace Conference, Vol. 6, 2000, pp. 449-455.
-
(2000)
Proceedings of the IEEE Aerospace Conference
, vol.6
, pp. 449-455
-
-
Larder, B.1
Azzam, H.2
Trammel, C.3
Vossler, G.4
-
3
-
-
0034849324
-
HUMS - The benefits- Past, Present and Future
-
Land. J.E., HUMS - The benefits- Past, Present and Future, Proceedings of the IEEE Aerospace Conference, Vol. 6, 2001, pp. 3083-3094.
-
(2001)
Proceedings of the IEEE Aerospace Conference
, vol.6
, pp. 3083-3094
-
-
Land, J.E.1
-
5
-
-
0141877261
-
-
Kluwer Academic Publishers, Dordrecht, The Netherlands
-
Vlot, A., Glare, history of the development of a new aircraft material, Kluwer Academic Publishers, Dordrecht, The Netherlands. 2001.
-
(2001)
Glare, history of the development of a new aircraft material
-
-
Vlot, A.1
-
6
-
-
0009339803
-
-
Kluwer Academic Publishers, Dordrecht, The Netherlands
-
Vlot, A., Gunnink, J.W., Fibre Metal Laminates, an introduction, Kluwer Academic Publishers, Dordrecht, The Netherlands, 2001.
-
(2001)
Fibre Metal Laminates, an introduction
-
-
Vlot, A.1
Gunnink, J.W.2
-
7
-
-
34547502692
-
Towards Technology Readiness of Fibre Metal Laminates - GLARE Technology Development 1997-2000
-
Harrogate, United Kingdom
-
nd International Congress of Aeronautical Sciences, Harrogate, United Kingdom, 2000, pp. 1-15.
-
(2000)
nd International Congress of Aeronautical Sciences
, pp. 1-15
-
-
Vlot, A.1
-
8
-
-
1642379628
-
Design of the Blended Wing Body Subsonic Transport
-
January-February
-
Liebeck, R.H., Design of the Blended Wing Body Subsonic Transport, Journal of Aircraft, Vol. 41, No. 1, January-February 2004, pp. 10-25.
-
(2004)
Journal of Aircraft
, vol.41
, Issue.1
, pp. 10-25
-
-
Liebeck, R.H.1
-
10
-
-
34547539821
-
-
The Blended-Wing Body, NASA Facts, FS-1997-07-24-LaRC July 1997.
-
The Blended-Wing Body, NASA Facts, FS-1997-07-24-LaRC July 1997.
-
-
-
-
11
-
-
33748070459
-
-
Ph.D. Dissertation, Virginia Polytechnic Institute and State University, Blacksburg, Virginia
-
Ko, .Y.A., The Multidisciplinary Design Optimization of a Distributed Propulsion Blended-Wing-Body Aircraft, Ph.D. Dissertation, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, 2003.
-
(2003)
The Multidisciplinary Design Optimization of a Distributed Propulsion Blended-Wing-Body Aircraft
-
-
Ko, Y.A.1
-
12
-
-
34547553196
-
-
Miller, M., Rufin, A.C., Westre, W.N., Samavedam, G., High-speed Civil Transport Hybrid Laminate Sandwich Fuselage Panel Test, Fatigue and Fracture Mechanics: Twenty-Ninth ASTM STP 1332 American Society for Testing and Materials, West Conshohocken, PA 1999.
-
Miller, M., Rufin, A.C., Westre, W.N., Samavedam, G., High-speed Civil Transport Hybrid Laminate Sandwich Fuselage Panel Test, Fatigue and Fracture Mechanics: Twenty-Ninth Volume, ASTM STP 1332 American Society for Testing and Materials, West Conshohocken, PA 1999.
-
-
-
-
13
-
-
0017023793
-
Design Study of Structural Concepts for an Arrow-Wing Supersonic Cruise Aircraft
-
Sakata, I.F., Davis. G.W., Robinson, J.C., Yates, E.C., "Design Study of Structural Concepts for an Arrow-Wing Supersonic Cruise Aircraft", Journal of Aircraft, Vol. 13, No. 11, 1976, pp. 880-888.
-
(1976)
Journal of Aircraft
, vol.13
, Issue.11
, pp. 880-888
-
-
Sakata, I.F.1
Davis, G.W.2
Robinson, J.C.3
Yates, E.C.4
-
14
-
-
34547538873
-
Airbus A300 Fuselage Program for Life Extension & Widespread Fatigue Damage Evaluation
-
Schmidt, H.J., Schmidt-Brandecker, B., Trey, H., Airbus A300 Fuselage Program for Life Extension & Widespread Fatigue Damage Evaluation, Proceedings of the Aging Aircraft Conference, Albuquerque, September 20-23, 1999 [online].
-
Proceedings of the Aging Aircraft Conference, Albuquerque, September 20-23, 1999 [online]
-
-
Schmidt, H.J.1
Schmidt-Brandecker, B.2
Trey, H.3
-
15
-
-
34547502375
-
-
Damage tolerance and fatigue evaluation of structure, Federal Aviation Regulations Part 25 - Airworthiness standards: Transport Category airplanes, Section 25.571, Federal Aviation Administration, Department of Transportation, Washington D.C., 1997.
-
Damage tolerance and fatigue evaluation of structure, Federal Aviation Regulations Part 25 - Airworthiness standards: Transport Category airplanes, Section 25.571, Federal Aviation Administration, Department of Transportation, Washington D.C., 1997.
-
-
-
-
16
-
-
31944445093
-
-
Woodhead Publishing Limited, Abington
-
Harris, B.. Fatigue in Composites, Woodhead Publishing Limited, Abington. 2003.
-
(2003)
Fatigue in Composites
-
-
Harris, B.1
-
17
-
-
0030126218
-
Impact Loading on Fibre Metal Laminates
-
VlOt, A., Impact Loading on Fibre Metal Laminates, Int. J. Impact Engng, Vol. 18, No. 3, pp. 291 307, 1996.
-
(1996)
Int. J. Impact Engng
, vol.18
, Issue.3
, pp. 291-307
-
-
VlOt, A.1
-
18
-
-
84878484390
-
Health monitoring of aircraft fuselage structures using ultrasonic waves
-
Hamburg
-
Zhou, Z. Q., Chiu, W. K., Bannister, M. K., Health monitoring of aircraft fuselage structures using ultrasonic waves, Proceedings of the 25th International Congress of the Aeronautical Sciences, Hamburg, 2006.
-
(2006)
Proceedings of the 25th International Congress of the Aeronautical Sciences
-
-
Zhou, Z.Q.1
Chiu, W.K.2
Bannister, M.K.3
-
19
-
-
34547509956
-
Aramid Reinforced ALuminium Laminates: Arall, Adhesion problems and environmental effects
-
Ph.D. Dissertation, Delft University of Technology, Delft
-
Verbruggen, M.L.C.E., "Aramid Reinforced ALuminium Laminates: Arall, Adhesion problems and environmental effects", Ph.D. Dissertation, Delft University of Technology, Delft, 1987.
-
(1987)
-
-
Verbruggen, M.L.C.E.1
-
20
-
-
0003598657
-
Fatigue Crack Growth in ARALL, A hybrid Aluminium-Aramid Composite Material, crack growth mechanisms and quantitative predictions of the crack growth rate
-
Ph.D. Dissertation, Delft University of Technology, Delft
-
Marissen, R., "Fatigue Crack Growth in ARALL, A hybrid Aluminium-Aramid Composite Material, crack growth mechanisms and quantitative predictions of the crack growth rate", Ph.D. Dissertation, Delft University of Technology, Delft, 1988.
-
(1988)
-
-
Marissen, R.1
-
21
-
-
0003679362
-
Towards GLARE - The Development of a fatigue insensitive and damage tolerant aircraft material
-
Ph.D. Dissertation, Delft University of Technology, Delft
-
Roebroeks, G.H.J J., "Towards GLARE - The Development of a fatigue insensitive and damage tolerant aircraft material", Ph.D. Dissertation, Delft University of Technology, Delft, 1991.
-
(1991)
-
-
Roebroeks, G.H.J.J.1
-
22
-
-
34547551955
-
-
A380: FLYING 21ST CENTURY TECHNOLOGY, Airbus Press release, May 2004
-
A380: FLYING 21ST CENTURY TECHNOLOGY, Airbus Press release, May 2004.
-
-
-
-
23
-
-
0020268746
-
Application of a new hybrid material (ARALL) in aircraft structures
-
Gunnink, J.W., Vogelesang, L.B., Schijve, J., Application of a new hybrid material (ARALL) in aircraft structures, Proceedings of the Congress of the International Council of the Aeronautical Sciences, 1982, pp. 990-1000.
-
(1982)
Proceedings of the Congress of the International Council of the Aeronautical Sciences
, pp. 990-1000
-
-
Gunnink, J.W.1
Vogelesang, L.B.2
Schijve, J.3
-
24
-
-
0030694899
-
-
American Institute of Aeronautics and Astronautics AIAA
-
Langelaan, J.W., Kok, L.J.J., "Damage Tolerance Modelling of Fibre/Metal Laminate Fuselage Structures", American Institute of Aeronautics and Astronautics AIAA, Vol. 4, 1997, pp. 2809-2818.
-
(1997)
Damage Tolerance Modelling of Fibre/Metal Laminate Fuselage Structures
, vol.4
, pp. 2809-2818
-
-
Langelaan, J.W.1
Kok, L.J.J.2
-
26
-
-
0031704781
-
Fatigue damage in titanium-graphite hybrid laminates
-
Collection of Technical Papers, AIAA/ASME/ASCE/AHS/ASC Structures
-
Burianek, Dennis A., Spearing, S. Mark, Fatigue damage in titanium-graphite hybrid laminates, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 3, pp. 2088-2097, 1998.
-
(1998)
Structural Dynamics and Materials Conference
, vol.3
, pp. 2088-2097
-
-
Burianek, D.A.1
Spearing, S.M.2
-
27
-
-
0842311515
-
-
Liu, Y.-L., A study on the fiber metal laminated panel for blast-resistant container, Proceedings of the International SAMPE Symposium and Exhibition, 48 II, pp. 2405-2413, 2003.
-
Liu, Y.-L., A study on the fiber metal laminated panel for blast-resistant container, Proceedings of the International SAMPE Symposium and Exhibition, 48 II, pp. 2405-2413, 2003.
-
-
-
-
29
-
-
33748685964
-
Ten Common Mistakes in Composite Design and Manufacture and How to Avoid Them
-
September/October
-
Peters, S.T., Ten Common Mistakes in Composite Design and Manufacture and How to Avoid Them, SAMPE Journal, Vol. 42, No., 5, September/October, 2006, pp. 53-59.
-
(2006)
SAMPE Journal
, vol.42
, Issue.and 5
, pp. 53-59
-
-
Peters, S.T.1
-
30
-
-
3042799366
-
Mode II delamination toughness of z-pinned laminates
-
Yan, W., Liu, H.Y., Mai, Y.W., Mode II delamination toughness of z-pinned laminates. Composites Science and Technology, Vol. 64, 2004, pp. 1937-1945.
-
(2004)
Composites Science and Technology
, vol.64
, pp. 1937-1945
-
-
Yan, W.1
Liu, H.Y.2
Mai, Y.W.3
-
31
-
-
6444234247
-
Delamination resistant laminates by Z-Fiber® pinning: Part I manufacture and fracture performance
-
Partridge, I.K., Cartié, D.D.R., Delamination resistant laminates by Z-Fiber® pinning: Part I manufacture and fracture performance, Composites: Part A, Vol. 36, 2005, pp. 55-64.
-
(2005)
Composites: Part A
, vol.36
, pp. 55-64
-
-
Partridge, I.K.1
Cartié, D.D.R.2
-
32
-
-
33644664978
-
Delamination of Z-pinned carbon fibre reinforced laminates
-
Cartié, D.D.R., Troulis. M., Partridge, I.K., Delamination of Z-pinned carbon fibre reinforced laminates, Composites Science and Technology, Vol. 66, 2006, pp. 855-861.
-
(2006)
Composites Science and Technology
, vol.66
, pp. 855-861
-
-
Cartié, D.D.R.1
Troulis, M.2
Partridge, I.K.3
-
33
-
-
33746102545
-
Properties of failure mechanisms of pinned composites lap joints in monotonie and cyclic tension
-
Chang, P., Mouritz, A.P., Cox, B.N., Properties of failure mechanisms of pinned composites lap joints in monotonie and cyclic tension, Composites Science and Technology, Vol. 66, 2006, pp. 2163-2176.
-
(2006)
Composites Science and Technology
, vol.66
, pp. 2163-2176
-
-
Chang, P.1
Mouritz, A.P.2
Cox, B.N.3
-
34
-
-
33748554902
-
Compression properties of z-pinned sandwich composites
-
Mouritz, A.P., Compression properties of z-pinned sandwich composites, Journal of Material Science, Vol. 41, 2006, pp. 5771-5774.
-
(2006)
Journal of Material Science
, vol.41
, pp. 5771-5774
-
-
Mouritz, A.P.1
-
35
-
-
33747167892
-
3D reinforcement of stiffener-to-skin T-joints by Z-pinning and tufting
-
Cartié, D.D.R., Dell'Anno, G., Poulin, E., Partridge, I.K., 3D reinforcement of stiffener-to-skin T-joints by Z-pinning and tufting, Engineering Fracture Mechanics, Vol. 73, 2006, pp. 2532-2540.
-
(2006)
Engineering Fracture Mechanics
, vol.73
, pp. 2532-2540
-
-
Cartié, D.D.R.1
Dell'Anno, G.2
Poulin, E.3
Partridge, I.K.4
-
37
-
-
0030150454
-
A history of fatigue
-
Schütz, W., A history of fatigue, Engineering Fracture Mechanics, Vol .54, Issue 2, pp. 263-300, 1996.
-
(1996)
Engineering Fracture Mechanics
, vol.54
, Issue.2
, pp. 263-300
-
-
Schütz, W.1
-
38
-
-
34547545558
-
Repair of Fibre Metal Laminates
-
Griffiths, G.R, McCarthy, R.F.J, Eds, France, pp
-
nd International SAMPE Europe Conference. Griffiths, G.R., McCarthy, R.F.J. (Eds.), France, pp. 63-74, 2001.
-
(2001)
nd International SAMPE Europe Conference
, pp. 63-74
-
-
Hooijmeijer, P.A.1
-
39
-
-
30344438821
-
Fatigue initiation in fibre metal laminates
-
April
-
Homan, J.J., Fatigue initiation in fibre metal laminates, International Journal of Fatigue, Volume 28. Issue 4. April 2006. Pages 366-374.
-
(2006)
International Journal of Fatigue
, vol.28
, Issue.4
, pp. 366-374
-
-
Homan, J.J.1
-
40
-
-
33745950625
-
Fatigue and damage tolerance issues of Glare in aircraft structures
-
October
-
Alderliesten, R.C., Homan, J.J., Fatigue and damage tolerance issues of Glare in aircraft structures, International Journal of Fatigue, Volume 28, Issue 10, October 2006, Pages 1116-1123.
-
(2006)
International Journal of Fatigue
, vol.28
, Issue.10
, pp. 1116-1123
-
-
Alderliesten, R.C.1
Homan, J.J.2
-
41
-
-
33845625682
-
Analytical prediction model for fatigue crack propagation and delamination growth in Glare
-
April
-
Alderliesten, R.C, Analytical prediction model for fatigue crack propagation and delamination growth in Glare, International Journal of Fatigue, Volume 29, Issue 4, April 2007, Pages 628-646.
-
(2007)
International Journal of Fatigue
, vol.29
, Issue.4
, pp. 628-646
-
-
Alderliesten, R.C.1
-
42
-
-
34547499755
-
-
Hinrichsen, J., Requirements for Care Free Aircraft Structures and expected benefits from Hybrid Structures/Materials, 65th Annual Conference of Society of Allied Weight Engineers, Valencia, CA 20-24 May 2006, SAWE Paper No. 3387.
-
Hinrichsen, J., Requirements for "Care Free" Aircraft Structures and expected benefits from Hybrid Structures/Materials", 65th Annual Conference of Society of Allied Weight Engineers, Valencia, CA 20-24 May 2006, SAWE Paper No. 3387.
-
-
-
-
43
-
-
13844299025
-
Durability of Glass Polymer Composites Subject to Stress Corrosion
-
Khennane, A., Melchers, R.E., Durability of Glass Polymer Composites Subject to Stress Corrosion, Journal of Composites for Construction, Vol. 7, No. 2, 2003, pp. 109-117.
-
(2003)
Journal of Composites for Construction
, vol.7
, Issue.2
, pp. 109-117
-
-
Khennane, A.1
Melchers, R.E.2
-
44
-
-
84902401441
-
The effect of aggressive environments on long-term behaviour
-
B. Harris Eds, Woodhead Publishing Limited, Abington, pp
-
Jones, F.R., The effect of aggressive environments on long-term behaviour, In: Fatigue in Composites, B. Harris (Eds.), Woodhead Publishing Limited, Abington, pp. 117-146, 2003.
-
(2003)
Fatigue in Composites
, pp. 117-146
-
-
Jones, F.R.1
-
45
-
-
0033742467
-
Development of fibre metal laminates for advanced aerospace structures
-
Vogelesang, L.B., Vlot, A., Development of fibre metal laminates for advanced aerospace structures, Journal of Materials Processing Technology 103, pp. 1-5, 2000.
-
(2000)
Journal of Materials Processing Technology
, vol.103
, pp. 1-5
-
-
Vogelesang, L.B.1
Vlot, A.2
-
46
-
-
0141973095
-
Static Properties of Fibre Metal Laminates
-
Hagenbeek, M., Hengel, C. van, Bosker, O.J., Vermeeren, C.A.J.R., Static Properties of Fibre Metal Laminates, Applied Composite Materials 10: 207-222, 2003.
-
(2003)
Applied Composite Materials
, vol.10
, pp. 207-222
-
-
Hagenbeek, M.1
Hengel2
van, C.3
Bosker, O.J.4
Vermeeren, C.A.J.R.5
|