Regulation Scheme of Turbofan Engine Nozzle for Infrared Signature Management

Author:

Chen MingORCID,Zhang Haibo

Funder

National Science and Technology Major Project

Publisher

Springer Science and Business Media LLC

Reference28 articles.

1. Liu Y, Liang C, Shi L (2021) Overall design of aviation gas turbine engines. Science Press, Beijing

2. Cheng W, Zhou L, Wang Z, Sun X, Shi J (2018) Effects of geometric parameters on infrared signature of serpentine nozzle. J Propul Technol 39(9):1974–1985

3. Sang X (2019) Research on some problems of infrared characteristics and stealth technology of aero-engine exhaust system. Nanjing University of Aeronautics and Astronautics

4. Shi X-J, Ji H (2020) Numerical investigation of influence of two-dimensional convergent and divergent nozzle’s design parameters on infrared characteristics. J Aerosp Power 35(5):12

5. Kim SJ, Kim YR, Kim Y, Kim MH, Lee M (2020) 2D exhaust nozzle with multiple composite layers for IR signature suppression. Results Phys 19:103395

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