Simplified Numerical Approach for the Prediction of Aerodynamic Forces on Grid Fins-Reference-Cited by-同舟云学术

Simplified Numerical Approach for the Prediction of Aerodynamic Forces on Grid Fins

Published:2018-07 Issue:4 Volume:55 Page:887-898
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Dikbas Erdem¹,Baran Özgür Uğraş²,Sert Cuneyt³

Affiliation:

1. TÜBİTAK SAGE, 06261 Ankara, Turkey

2. TED University, 06420 Ankara, Turkey

3. Middle East Technical University, 06800 Ankara, Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34062

Reference18 articles.

1. BelotserkovskyS. M.OdnovolL. A.SafinY. Z.TylenevA. I.FrolovV. P.ShitovV. A., Reshetchatye Krylya (Lattice Wings), Mashinostroenie, Moscow, 1985, pp. 10–96 (in Russian).

2. Nonlinear aerodynamic analysis of grid fin configurations

3. Grid Fin Aerodynamics for Missile Applications in Subsonic Flow

4. Aerodynamic Characterization of Grid Fins at Subsonic Speeds

5. Aerodynamic Analysis of Grid-Fin Configurations at Supersonic Speeds

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