Author:
Kaya Ufuk,Oksuztepe Eyyup
Publisher
Springer International Publishing
Reference8 articles.
1. Ferreira, C. A., & Richter, E. (1993). Detailed design of a 250-kW switched reluctance starter/generator for an aircraft engine. SAE Transactions, 289–300. https://doi.org/10.4271/931389
2. Friedrich, G., & Girardin, A. (2009). Integrated starter generator. IEEE Industry Applications Magazine, 15(4), 26–34.
3. Ganev, E. (2014). Selecting the best electric machines for electrical power-generation systems: High-performance solutions for aerospace more electric architectures. IEEE Electrification Magazine, 2(4), 13–22.
4. International Council on Clean Transportation. (2018). https://theicct.org/sites/default/files/publications/ICCT_CO2-commercl-aviation-2018_20190918.pdf. Accessed on 22 Sept 2021.
5. Ismagilov, F. R., & Vavilov, V. E. (2019). Optimization of a high-temperature starter—Generator of inverted design for aircraft. Russian Electrical Engineering, 90(5), 391–396.