Cite this DOI

Dr. B.S. R. Murthy (2017). Thermal Stress Analysis of PEEK Fiber Composites at Cryogenic Temperature. *Journal of Science & Technology*, *02*(03), 11–12. https://doi.org/10.46243/jstj.2017.v2.i3.123

@article{drbsrmurthy2017thermal,
  author    = {Dr. B.S. R. Murthy},
  title     = {{Thermal Stress Analysis of PEEK Fiber Composites at Cryogenic Temperature}},
  journal   = {Journal of Science \& Technology},
  year      = {2017},
  month     = {may},
  volume    = {02},
  number    = {03},
  pages     = {11--12},
  publisher = {Longman Publishers},
  issn      = {2456-5660},
  doi       = {10.46243/jstj.2017.v2.i3.123},
  url       = {https://doi.org/10.46243/jstj.2017.v2.i3.123},
  language  = {en},
  abstract  = {Fiber reinforced composites are class of materials that are workable engineering materials possessing high strength to weight ratio resulting in reduction of weight and hence savings in energy. Composites can be tailor -made to the required duty by changing the nature and proportion of the constituent materials. Composites exhibit anisotropy in mechanical and thermal properties. This makes the design of composite structures more complex and demanding. Composites have wide applications as supports and structures at cryogenic temperatures in super conducting magnets and as fuel tankage in spacecraft and rocketry. As these composites are fabricated at 1000 C to 2000 C, \textasciitilde{} their use at low temperatures creates thermal stresses. They become brittle at low temperatures and thermal strain of matrix ma:f be of the same order of the ultimate tensile strain at helium temperature (4.2K); thus leaving no more load bearingcapability}
}

TY  - JOUR
TI  - Thermal Stress Analysis of PEEK Fiber Composites at Cryogenic Temperature
AU  - Dr. B.S. R. Murthy
JO  - Journal of Science & Technology
PY  - 2017
DA  - 2017/05/04/
VL  - 02
IS  - 03
SP  - 11
EP  - 12
PB  - Longman Publishers
SN  - 2456-5660
LA  - en
AB  - Fiber reinforced composites are class of materials that are workable engineering materials possessing high strength to weight ratio resulting in reduction of weight and hence savings in energy. Composites can be tailor -made to the required duty by changing the nature and proportion of the constituent materials. Composites exhibit anisotropy in mechanical and thermal properties. This makes the design of composite structures more complex and demanding. Composites have wide applications as supports and structures at cryogenic temperatures in super conducting magnets and as fuel tankage in spacecraft and rocketry. As these composites are fabricated at 1000 C to 2000 C, ~ their use at low temperatures creates thermal stresses. They become brittle at low temperatures and thermal strain of matrix ma:f be of the same order of the ultimate tensile strain at helium temperature (4.2K); thus leaving no more load bearingcapability
DO  - 10.46243/jstj.2017.v2.i3.123
UR  - https://doi.org/10.46243/jstj.2017.v2.i3.123
ER  -

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    "id": "10.46243/jstj.2017.v2.i3.123",
    "DOI": "10.46243/jstj.2017.v2.i3.123",
    "URL": "https://doi.org/10.46243/jstj.2017.v2.i3.123",
    "title": "Thermal Stress Analysis of PEEK Fiber Composites at Cryogenic Temperature",
    "source": "Smart Scholars DOI Registry",
    "container-title": "Journal of Science & Technology",
    "author": [
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            "family": "Dr. B.S. R. Murthy"
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    "volume": "02",
    "issue": "03",
    "page": "11-12",
    "publisher": "Longman Publishers",
    "language": "en",
    "abstract": "Fiber reinforced composites are class of materials that are workable engineering materials possessing high strength to weight ratio resulting in reduction of weight and hence savings in energy. Composites can be tailor -made to the required duty by changing the nature and proportion of the constituent materials. Composites exhibit anisotropy in mechanical and thermal properties. This makes the design of composite structures more complex and demanding. Composites have wide applications as supports and structures at cryogenic temperatures in super conducting magnets and as fuel tankage in spacecraft and rocketry. As these composites are fabricated at 1000 C to 2000 C, ~ their use at low temperatures creates thermal stresses. They become brittle at low temperatures and thermal strain of matrix ma:f be of the same order of the ultimate tensile strain at helium temperature (4.2K); thus leaving no more load bearingcapability",
    "ISSN": "2456-5660"
}

From the record as registered (version 2) — the record and its history. Programs: https://registry.smartscholars.in/api.php?action=cite&doi=10.46243%2Fjstj.2017.v2.i3.123 gives all four in one JSON answer.