Grid fins for missile applications in supersonic flow

Author:

Burkhalter John1

Affiliation:

1. Auburn Univ., AL

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Belotserkovskiy, S. M., Odnovol, L. A., etal, "Wings With Internal Framework", Machine Translation, FTD-DD(RS)T-1289-86, Foreign Technology Division,Feb. 87.

2. Nonlinear aerodynamic analysis of grid fin configurations

3. Kuethe, A. M., and Chow, C.Y., Foundations of Aerodynamics. John Wiley and Sons, New York, FourthEdition,1986, pp222-236.

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1. Prediction of Aerodynamic Characteristics of the Grid Fins using Low/High Fidelity Methods;Journal of the Korea Institute of Military Science and Technology;2023-04-05

2. Parametric Design and Investigation of Grid Fin Aerodynamics in Supersonic Flow using Computational Fluid Dynamics;AIAA AVIATION 2022 Forum;2022-06-20

3. Integration of Grid Fins for the Optimal Design of Missile Systems;AIAA Atmospheric Flight Mechanics Conference;2015-01-02

4. CFD Simulation of grid fin flows;31st AIAA Applied Aerodynamics Conference;2013-06-22

5. Aerodynamic Characterization of Grid Fins at Subsonic Speeds;Journal of Aircraft;2007-03

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