Abstract
Grid fins are unconventional lifting and control surfaces consisting of an outer frame supporting an inner grid of intersecting small chord planar surfaces. Cascade fins are a new category of grid fins. Unlike grid fins, cascade fins do not have cross members. In the present work, a sequence of simulation results obtained for comparative analysis of cascade fins versus flat plate (FP) for different angles of attack (\(\alpha \)) is presented. The results indicate an overall increase in lift force compared to flat plates at all angles. The results are in agreement with the experimental data and indicate that cascading effect leads to a delay in flow separation and thus delayed stall.
References
Ariff M, Salim SM, Cheah SC (2009) Wall y\(^+\) approach for dealing with turbulent flow over a surface mounted cube: part 1-low reynolds number. In: Proceedings of seventh international conference on CFD in the minerals and process industries, Melbourne, Australia
Belotzerkovsky SM (1987) Wings with internal framework. In: Machine translation, FTD-ID (RS) T-1289-86, Foreign Technology Div
CFD++ 15.1.1 (2015) CFD++ user manual
Eugene LF (2001) Tactical missile design. In: AIAA education series, pp 1–18
Ledlow TI, Burkhalter JE, Hartfield RJ (2015) Integration of grid fins for the optimal design of missile systems. In: AIAA atmospheric flight mechanics conference
Menter FR (1994) Two-equation eddy-viscosity turbulence models for engineering applications. AIAA J 32(8):1598–1605
Misra A (2009) Investigation of grid and cascade fins for missile flight stabilization and control. Ph.D. Thesis. In: Indian institute of technology, Kanpur, India
Misra A, Ghosh AK, Ghosh K (2008) Cascade fins—an alternate tail stabilization unit. In: AIAA atmospheric flight mechanics conference and exhibit, vol 6884. Honolulu, Hawaii
Misra A, Ghosh AK, Ghosh K (2008) Stability and control of aircraft bombs at high angle of attack using cascade fins. In: NCAAT proceedings, pp S1.3/1–S1.3/7
Miller MS, Washington WD (1998) Experimental investigations of grid fin aerodynamics: a synopsis of nine wind tunnel and three fight tests. In: Proceedings of the NATO research proposal, Page 21 RTO-MP-5. Missile aerodynamics, NATO research and technology organization
Miller MS, Washington WD (1993) Curvature and leading edge sweep back effects on grid fin aerodynamic characteristics. AIAA
MIME User Manual (2015) Metacomp technologies
Munawar S (2010) Analysis of grid fins as efficient control surface in comparison to conventional planar fins. In: 27th International congress of the aeronautical sciences
NWTF Faculty & Management. http://www.iitk.ac.in/infocell/flier/nwtf1.pdf
Salim SM, Cheah S (2009) Wall y\(^+\) strategy for dealing with wall-bounded turbulent flows. In: Proceedings of the international multiconference of engineers and computer scientists, Hong Kong
SpaceX Falcon 9. http://www.spacex.com/falcon9
Spalart PR, Allmaras SR (1992) A one-equation turbulence model for aerodynamic flows. In: AIAA 30th aerospace sciences meeting and exhibit, Reno, NV, USA
Zaloga S (2000) The Scud and other Russian Ballistic Missiles, New Territories. Concord Publications Co., Hong Kong
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Tripathi, M., Mahesh, M.S., Misra, A. (2018). High Angle of Attack Analysis of Cascade Fin in Subsonic Flow. In: Singh, S., Raj, P., Tambe, S. (eds) Proceedings of the International Conference on Modern Research in Aerospace Engineering. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-10-5849-3_13
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DOI: https://doi.org/10.1007/978-981-10-5849-3_13
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