Induced Aerodynamics of Wrap-Around Fins Using an Empirical Technique

Author:

Wilks Brett1

Affiliation:

1. U.S. Army Aviation and Missile Research, Developmont and Engineering Center

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. cr ct Lref Sref θ R AR λ b/2 Λ Sp Sw F010 4.2500 4.2500 4.2500 12.75 0.0 ∞ 1.4118 1.0 3.000 0.0 12.7500 12.7500 F012 " " " " 45.0 3.9197 1.4118 " " 0.0 " 13.0837 F014 " " " " 90.0 2.1213 1.4118 " " 0.0 " 14.1616 F016 " " " " 135.0 1.6236 1.4118 " " 0.0 " 16.2584 F018 " " " " 180.0 1.5000 1.4118 " " 0.0 " 20.0277

2. F020 3.0000 3.0000 3.0000 12.75 0.0 ∞ 2.8333 1.0 4.250 0.0 12.7500 12.7500 F024 " " " " 90.0 3.0052 2.8333 " " 0.0 " 14.1617 F026 " " " " 135.0 2.3001 2.8333 " " 0.0 " 16.2584

3. F030 4.9100 2.4550 3.6825 12.75 0.0 ∞ 1.8824 0.5 3.466 35.0 12.7635 12.7635 F034 " " " " 90.0 2.4508 1.8824 " " 35.0 " 14.1765 F036 " " " " 135.0 1.8758 1.8824 " " 35.0 " 16.2757 F040 3.6825 3.6825 3.6825 12.75 0.0 ∞ 1.8824 1.0 3.466 0.0 12.7635 12.7635 F044 " " " " 90.0 2.4508 1.8824 " " 0.0 " 14.1765

4. As seen in Figure 6

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