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Hirotaka Igawa

The following bibliography contains all publications indexed in this database that are linked with this name as either author, editor or any other kind of contributor.

  1. Kobayashi, Makito / Ogino, Hideharu / Burman, Magnus / Wada, Daichi / Igawa, Hirotaka / Murayama, Hideaki (2023): Shape sensing for CFRP and aluminum honeycomb sandwich panel using inverse finite element method with distributed fiber-optic sensors. In: Composite Structures, v. 308 (March 2023).

    https://doi.org/10.1016/j.compstruct.2022.116648

  2. Murayama, Hideaki / Kageyama, Kazuro / Uzawa, Kiyoshi / Ohara, Kohei / Igawa, Hirotaka (2011): Strain monitoring of a single-lap joint with embedded fiber-optic distributed sensors. In: Structural Health Monitoring, v. 11, n. 3 (August 2011).

    https://doi.org/10.1177/1475921711419994

  3. Wada, Daichi / Igawa, Hirotaka / Tamayama, Masato / Kasai, Tokio / Arizono, Hitoshi / Murayama, Hideaki (2019): Flight demonstration of aircraft wing monitoring using optical fiber distributed sensing system. In: Smart Materials and Structures, v. 28, n. 5 (May 2019).

    https://doi.org/10.1088/1361-665x/aae411

  4. Ning, Xiaoguang / Murayama, Hideaki / Kageyama, Kazuro / Wada, Daichi / Kanai, Makoto / Ohsawa, Isamu / Igawa, Hirotaka (2014): Dynamic strain distribution measurement and crack detection of an adhesive-bonded single-lap joint under cyclic loading using embedded FBG. In: Smart Materials and Structures, v. 23, n. 10 (October 2014).

    https://doi.org/10.1088/0964-1726/23/10/105011

  5. Wada, Daichi / Igawa, Hirotaka / Tamayama, Masato / Kasai, Tokio / Arizono, Hitoshi / Murayama, Hideaki / Shiotsubo, Katsuya (2018): Flight demonstration of aircraft fuselage and bulkhead monitoring using optical fiber distributed sensing system. In: Smart Materials and Structures, v. 27, n. 2 (February 2018).

    https://doi.org/10.1088/1361-665x/aaa588

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