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Prediction of Aerodynamic Stability Derivatives of Shell Configuration of Missile Using CFD Method
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J. KIMS Technol. 2020;23(4):363-370. Published online 2020 Aug 5 DOI: https://doi.org/10.9766/KIMST.2020.23.4.363
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Citations to this article as recorded by
 Investigation of pitching frequency impact on stability criteria for supersonic fin stabilized missile
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