Computational Fluid Dynamics and Experimental Data Comparison of a Missile-Model Roll Derivative
| العنوان: | Computational Fluid Dynamics and Experimental Data Comparison of a Missile-Model Roll Derivative |
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| المؤلفون: | Saša Živković, Mirko Kozić, Marija Samardžić, Habib Belaidouni |
| المصدر: | Journal of Spacecraft and Rockets. 54:672-682 |
| بيانات النشر: | American Institute of Aeronautics and Astronautics (AIAA), 2017. |
| سنة النشر: | 2017 |
| مصطلحات موضوعية: | Physics, 020301 aerospace & aeronautics, Angle of attack, business.industry, Courant–Friedrichs–Lewy condition, Aerospace Engineering, 02 engineering and technology, Mechanics, Computational fluid dynamics, 01 natural sciences, 010305 fluids & plasmas, Physics::Fluid Dynamics, Flow separation, Missile, 0203 mechanical engineering, Computer Science::Systems and Control, Space and Planetary Science, Control theory, 0103 physical sciences, Supersonic speed, Reynolds-averaged Navier–Stokes equations, business, Transonic, Astrophysics::Galaxy Astrophysics |
| الوصف: | The roll damping dynamic stability derivative for a modified basic finner missile at transonic and supersonic speeds is calculated using quasi-stationary and unsteady computational fluid dynamics m... |
| تدمد: | 1533-6794 0022-4650 |
| DOI: | 10.2514/1.a33674 |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=doi_________::29c2c72b2b7a0e27c68db37266af88f4 https://doi.org/10.2514/1.a33674 |
| رقم الانضمام: | edsair.doi...........29c2c72b2b7a0e27c68db37266af88f4 |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 15336794 00224650 |
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| DOI: | 10.2514/1.a33674 |