To Test the Smart Sensors for AIAA
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-8394-8_5
Reference12 articles.
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2. Verrilli, M., Calomino, A., Thomas, D.J., Robinson, R.C.: Characterization of ceramic matrix composite vane subelements subjected to rig testing in a gas turbine environment. In: Fifth International Conference on High Temperature Ceramic Matrix Composites, Seattle, WA, USA, Sept 2004 (2004)
3. Padture, N.P.: Advanced structural ceramics in aerospace propulsion. Nat. Mater. 15(8), 804–809 (2016). https://doi.org/10.1038/nmat4687
4. Hunter, G.W., Neudeck, P.G., Okojie, R.S., Beheim, G.M., Powell, J.A., Chen, L.: An overview of high-temperature electronics and sensor development at NASA Glenn Research Center. J. Turbomach. 125(4), 658–664 (2003). https://doi.org/10.1115/1.1579508
5. Franklin, L.D., Li, J., Gao, J., Ding, G., Cao, X.: Integrated fabrication of high-temperature microelectromechanical system sensor on aeroengine turbine blade. J. Thermophys. Heat Transfer 32(3), 828–830 (2018). https://doi.org/10.2514/1.T5147
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