Flow Characteristics Study on Aerospike Nozzle for Varying Lengths Using CFD Method
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-4500-5_5
Reference15 articles.
1. Tokoh K, Oyama A, Tomita T, Negishi H (2023) Multiobjective aerodynamic design optimization of the contour of annular aerospike nozzles. In AIAA SCITECH 2023 forum, p 1470
2. Tobias JR, Agrawal AK (2023) Flow development in radial plane of rotating detonation engine integrated with aerospike. J Propul Power 39(3):318–330
3. Reza MdS, Agrawal BK, Tarnacha RS, Panchal D (2022) Computational investigation of the effect of variable cowl length on the flowfield of conical aerospike nozzles. Aerosp Syst 1–14
4. Liu X-Y, Cheng M, Zhang Y-Z, Wang J-P (2022) Design and optimization of aerospike nozzle for rotating detonation engine. Aerosp Sci Technol 120:107300
5. Mishra AK, Goswami V, Sarma P (2021) Aerodynamic thrust characteristics and performance valuations for an aerospike nozzle-review. Int J Eng Appl Sci Technol 5(11):128–133
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