CFD Study of Base Drag of the Grot Rocket
References
- [1] Gregorek, G.M. “Aerodynamic Drag of Model Rockets (TR-11).” Estes Industries, R&D 359-71. Penrose, Colorado, USA, 1970.
- [2] Moore, F.G., Hymer, T.C. and Wilcox, J.W. “Improved Empirical Model for Base Drag Prediction on Missile Configurations Based on New Wind Tunnel Data.” Naval Surface Warfare Center Dahlgren Division, AD-A258 753. Hampton, Virginia, USA, 1992.
- [3] Brazzel, C.E. and Henerson, J.H. “A Correlation of the Base Drag of Bodies-of-Revolution with a Jet Exhausting through the Base.” Army Missile Command, Redstone Arsenal, AD0634662. 1966.
- [4] Huffman, M. “Sounding Rocket Redesign and Optimization for Payload Expansion and in Flight Telemetry Transmittal.”, MSc thesis, University of Central Florida. Orlando, Florida, USA, 2005.
- [5] Al-Obaidi, A.S.M. “Implementation of Semi-Empirical Models to Enhance the Accuracy of Panel Methods for Drag Prediction at Supersonic Speeds.” IIUM Engineering Journal Vol. 12 No. 1 (2011): pp. 45–58.
- [6] Kumar, V.S. “Estimation of Base Drag on Supersonic Cruise Missile.” International Research Journal of Engineering and Technology Vol. 3 No. 1 (2016): pp. 662–665.
- [7] Sutton, G.P. and Biblarz, Oscar. Rocket Propulsion Elements. 9th edn. John Wiley & Sons, Inc Hoboken, New Jersey, USA, 2016.
- [8] Gordon, S. and McBride, B.J. Computer Program for Calculation of Complex Chemical Equilibrium CompoSitions and Applications. 1st edn. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, Springfield, Virginia, USA, 1994.
- [9] Çengel, Y.A. and Cimbala, J.M. Fluid Mechanics: Fundamentals and Applications. 3rd edn. McGraw Hill, New York, New York, USA, 2014.
- [10] López, D., Domínguez, D. and Gonzalo, J. “Impact of Turbulence Modelling on External Supersonic Flow Field Simulations in Rocket Aerodynamics.” International Journal of Computational Fluid Dynamics Vol. 27 No. 8–10 (2013): pp. 332–341.
- [11] Aytaç, Z. and Aktas, F. “Utilization of CFD for the Aerodynamic Analysis of a Subsonic Rocket.” Politeknik Dergisi Vol. 23 No. 3 (2020): pp. 879–887.
- [12] Ansys, Inc. ANSYS Fluent User’s Guide, Release 17. 2. 2016.
DOI: https://doi.org/10.2478/tar-2023-0007 | Journal eISSN: 2545-2835
Language: English
Page range: 1 - 16
Submitted on: Apr 24, 2022
Accepted on: Mar 2, 2023
Published on: Jun 12, 2023
Published by: Sciendo
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
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© 2023 Nezar Sahbon, Maciej Michałów, Siddharth Murpani, Paulina Żurawka, Kacper Kaczmarek, published by Sciendo
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