Design of rotation inducing rocket fins and their analysis for aerodynamic stability

Author:

Karlekar ChinmayORCID,Barve Shivprakash B.

Publisher

Springer Science and Business Media LLC

Reference11 articles.

1. Azevedo FS (2013) Knowing the stability of model rockets: a study of learning in interest-based practices. Cognition and Instruction. Routledge Informa Ltd, London, pp 345–374

2. Kobald M et al (2018) Hybrid experimental rocket stuttgart: a low-cost technology demonstrator. In: Proceedings of the Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics Inc. 55:1–17. 10.2514/1.A34035

3. Mishra AK et al (2021) Conceptual design and analysis of two stage sounding rocket. In: Presented at international conference on innovations in multidisciplinary research (ICIMR-2021) Held on 23rd and 24th August 2021

4. Smith E (1971) Autorotating wings: an experimental investigation. J Fluid Mech 50(3):513–534

5. Dahlke C, Madison W, Pettis A (1968) Fin for inducing spin in rotating rockets. United States Patent Office. 3(390):850

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