Numerical Investigations of Aerodynamics Performance of Blunt Nose Cone with Aerodisk at Hypersonic Flow-Reference-Cited by-同舟云学术

Numerical Investigations of Aerodynamics Performance of Blunt Nose Cone with Aerodisk at Hypersonic Flow

Published:2024 Issue: Volume: Page:177-188
ISSN:2522-8714
Container-title:Advances in Science, Technology & Innovation
language:en
Short-container-title:

Author:

Chauhan Jhanvi,Balaji G.,Swastikar Monika,Boopathy G.,Sangeetha S.,Santhosh Kumar G.,Pradeep G. M.

Publisher

Springer Nature Switzerland

Link

https://link.springer.com/content/pdf/10.1007/978-3-031-50024-4_18

Reference9 articles.

1. Balaji, G., Senthil Kumar, C., Nadaraja Pillai, S., & Senthil Kumar, R. (2015). Aerodynamic performance enhancement of blunt body using aero disk. International Journal of Applied Engineering Research, 10(33).

2. Balaji, G., Sree, K. N., Reddy, E. V., Sumanth, N., Sathish, S., & Madhanraj, V. (2022). Numerical investigation of flow over a hemispherical missile nose cone configuration in subsonic speed. Materials Today: Proceedings, 68, 1447–1454.

3. Deng, F., Jiao, Z., Liang, B., Xie, F., & Qin, N. (2017). Spike effects on drag reduction for hypersonic lifting body. Journal of Spacecraft and Rockets, 54(6), 1185–1195.

4. Elsamanoudy, M., Ghorab, A., & Hendy, M. (2013, May 28–30) Drag reduction using spiked-aerodisk & reattachment ring for hypersonic hemispherical bodies. In International Conference on Aerospace Sciences and Aviation Technology (Vol. 15). Aerospace Sciences & Aviation Technology, ASAT-15 (pp. 1–16). The Military Technical College.

5. Hamid, A. H. A., Salleh, Z., Suloh, A. M. I. M., Sujana, M. J., Saad, M. S., & Khamis, M. I. (2022). Evaluation of a newly designed aerodisk for cloud seeding prototype rocket drag reduction. Pertanika Journal of Science & Technology, 30(2)