Experimental and analytical analysis of grid fin configurations
Author:
Affiliation:
1. Rockwell International Missile Systems Division, Duluth, Georgia
2. Auburn University, Auburn, Alabama
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45856
Reference4 articles.
1. Erg�nzung zu dem Aufsatz von N. Scholz, Beitr�ge zur Theorie der tragenden Fl�che
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1. Wind Tunnel Study of a Grid Fin Stabilized Guided Projectile;Journal of Aerospace Sciences and Technologies;2023-08-07
2. Aeroelastic Stability of an Aerial Refueling Hose–Drogue System with Aerodynamic Grid Fins;Aerospace;2023-05-18
3. Experimental Study on Aerodynamic Characteristics for Missile Configuration With Grid Fins in Subsonic Flow;Journal of the Korean Society for Aeronautical & Space Sciences;2021-09-30
4. Effect of Chord Variation on Subsonic Aerodynamics of Grid Fins;Lecture Notes in Mechanical Engineering;2021
5. Effect of aspect ratio variation on subsonic aerodynamics of cascade type grid fin at different gap-to-chord ratios;The Aeronautical Journal;2019-12-03
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