Zobrazeno 1 - 9
of 9
pro vyhledávání: '"N. K. Gopinath"'
Publikováno v:
ACS Applied Materials & Interfaces. 11:47491-47500
Despite extensive research on developing different transition metal boride composites for aero-thermostructural applications, the understanding of the shockwave interaction using high pressure shoc...
Publikováno v:
Journal of the American Ceramic Society. 102:6925-6938
Publikováno v:
Spark Plasma Sintering of Materials ISBN: 9783030053260
The ultrahigh-temperature ceramics (UHTCs) have been considered as the emerging class of materials, suitable for the high-temperature (exceeding 2000 °C) structural applications in oxidation environment, including hypersonic aviation, rocket propuls
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea12f96b2b67cf2241f48f86a63d3715
https://doi.org/10.1007/978-3-030-05327-7_13
https://doi.org/10.1007/978-3-030-05327-7_13
Publikováno v:
Journal of the Ceramic Society of Japan. 124:393-402
Zirconium diboride based ceramics, owing to their superior high temperature properties are potential materials for use as leading edge components in hypersonic space vehicles. However, the difficulty in sintering these ultra high temperature ceramics
Autor:
Mahapatra D. R, N K Gopinath
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Autor:
Mahapatra D. R, N K Gopinath
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Publikováno v:
30th International Symposium on Shock Waves 1 ISBN: 9783319462110
Long endurance hypersonic air-breathing vehicles experience very high temperatures owing to the generation of shock waves and viscous dissipation. Extreme heat flux is experienced by the scramjet combustor due to exothermic combustion and requires me
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40ea6661a0e3079674d31980c6da8e55
https://doi.org/10.1007/978-3-319-46213-4_39
https://doi.org/10.1007/978-3-319-46213-4_39
Publikováno v:
30th International Symposium on Shock Waves 1 ISBN: 9783319462110
Hypersonic waveriders are attractive candidate for futuristic hypersonic air-breathing cruise vehicles, owing to high L/D ratio. Waveriders face extreme thermomechanical loads due to shock waves, air stagnation at leading edges, skin friction along t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42b17237fd5947a4f6238ea2ec992ba0
https://doi.org/10.1007/978-3-319-46213-4_41
https://doi.org/10.1007/978-3-319-46213-4_41
Publikováno v:
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.