Zobrazeno 1 - 10
of 859
pro vyhledávání: '"Carbon-carbon composite"'
Publikováno v:
Science and Engineering of Composite Materials, Vol 31, Iss 1, Pp 16641-6 (2024)
Needle-punched carbon/carbon (NP C/C) composites are widely used in thermal protection systems for aerospace engineering. Oxidation and ablation affect their mechanical properties at high temperatures of service environment. A thermo-mechanical coupl
Externí odkaz:
https://doaj.org/article/702165b51d934a8481545dab5d38add9
Autor:
Dipoo Kumar, Anil Painuly, Vinu Viswanath V, Krishnakumar G, Deepak Kumar Agarwal, Gomathi Nageswaran
Publikováno v:
Carbon Trends, Vol 16, Iss , Pp 100380- (2024)
Carbon-carbon composite manufactured by deposition of pyrocarbon (PyC) through chemical vapor infiltration (CVI) has the key issue of being process parametric sensitive which necessitates the detailed study of the effect of process parameters on the
Externí odkaz:
https://doaj.org/article/d525b5bd134e430b872caffacd58e42f
Autor:
Nilesh Agarwal, Aditya Rangamani, Kathan Bhavsar, Shreyash Santosh Virnodkar, Aldrin Antonio Agostinho Fernandes, Utkarsh Chadha, Divyansh Srivastava, Albert E. Patterson, Vezhavendhan Rajasekharan
Publikováno v:
Frontiers in Materials, Vol 11 (2024)
Carbon-carbon composites are advanced materials known for their high strength, high-temperature stability, and superior thermal conductivity. Mechanical properties such as tensile strength, flexural strength, and compressive strength are examined, as
Externí odkaz:
https://doaj.org/article/619f397017c04e4ebd756e4b56b50847
Autor:
Behrooz Shahriari, Keyvan Shojaei
Publikováno v:
Mechanics of Advanced Composite Structures, Vol 10, Iss 2, Pp 271-282 (2023)
The correct materials selection in the design of aerospace structures reduces the weight and increases structural efficiency. Since the rotor in gas turbine engines has a significant weight, it is important to reduce its weight. The rotating disks in
Externí odkaz:
https://doaj.org/article/a984191ddfeb4f2c8f79f8fe796496fd
Autor:
Andrea Delfini, Roberto Pastore, Marta Albano, Fabio Santoni, Fabrizio Piergentili, Mario Marchetti
Publikováno v:
Applied Sciences, Vol 14, Iss 13, p 5850 (2024)
Atomic oxygen (AtOx) is a major component of the space environment between 200 and 800 km (LEO—low Earth orbit region) and is the principal source of erosion for exposed aerospace structures. The damage to surface materials is proportional to the A
Externí odkaz:
https://doaj.org/article/471e5b7260024892a1bf7d4273800800
Autor:
Chamaal Karunaweera, Nimanka P. Panapitiya, Samitha Panangala, Edson V. Perez, Inga H. Musselman, Kenneth J. Balkus, John P. Ferraris
Publikováno v:
Separations, Vol 11, Iss 4, p 108 (2024)
The use of immiscible polymer blends in gas separations is limited due to uncontrollable phase separation. In contrast, compatibilized immiscible polymer blends can be used as precursors with controlled morphologies that allow for a unique pore archi
Externí odkaz:
https://doaj.org/article/6c2af27dd3084ab6bd2eb927f91de3d8
Publikováno v:
Science and Engineering of Composite Materials, Vol 29, Iss 1, Pp 508-515 (2022)
Needle-punched (NP) carbon/carbon composites (CCCs) are widely used in structures re-entering the atmosphere of aerospace, thanks to their excellent mechanical properties. They are easily oxidized at high temperatures with atmospheric oxygen. The oxi
Externí odkaz:
https://doaj.org/article/278e2f543eb34710a368de6ad62076f5
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