Alemdaroğlu, Hüseyin Nafiz

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https://hdl.handle.net/20.500.14411/7087
Name Variants
H.N.Alemdaroğlu
Huseyin Nafiz, Alemdaroglu
H.N.Alemdaroglu
A.,Hüseyin Nafiz
Alemdaroğlu, Hüseyin Nafiz
Alemdaroğlu,H.N.
H. N. Alemdaroglu
Alemdaroglu,H.N.
H., Alemdaroglu
A.,Huseyin Nafiz
A., Huseyin Nafiz
Alemdaroglu, Huseyin Nafiz
A., Hüseyin Nafiz
H. N. Alemdaroğlu
Hüseyin Nafiz, Alemdaroğlu
H.,Alemdaroğlu
Alemdaroğlu,N.
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Profesor Doktor
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nafiz.alemdaroglu@atilim.edu.tr
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Airframe and Powerplant Maintenance
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3

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1

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2

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1

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0.67

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1

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1

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2018 Applied Aerodynamics Conference -- 36th AIAA Applied Aerodynamics Conference, 2018 -- 25 June 2018 through 29 June 2018 -- [state] GA -- 2151091
2018 Fluid Dynamics Conference -- 48th AIAA Fluid Dynamics Conference, 2018 -- 25 June 2018 through 29 June 2018 -- Atlanta -- 2151391
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Author: Alemdaroğlu,N.

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    Citation - Scopus: 2
    Computational Fluid Dynamics Modelling of Store Separation for Transonic Generic Store
    (American Institute of Aeronautics and Astronautics Inc, AIAA, 2018) Demir,G.; Alemdaroğlu,N.
    In this study, two different well-known wind tunnel techniques; “Captive Trajectory Method “and “Grid Surveying Method “are simulated using Computational Fluid Dynamics (CFD) method. Time dependent behavior of a generic store during the release process from a delta wing under high transonic flow regime is determined. First of all, in captive trajectory simulation, simultaneous trajectory and attitude computations are accomplished by utilizing a reliable commercial flow solver called ANSYS Fluent. Secondly, aerodynamic grid database generation required for grid surveying approach is performed and the trajectory of the store is determined by using a standalone store separation module built in MATLAB Simulink. The numerical outputs are compared with available wind tunnel results conducted in Arnold Engineering Development Center. © 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.