Static Aeroelastic Modeling of a Sub-Scale Wind Tunnel Model with Novel Flap Concept-Reference-Cited by-同舟云学术

Static Aeroelastic Modeling of a Sub-Scale Wind Tunnel Model with Novel Flap Concept

Published:2015-01-02 Issue: Volume: Page:
ISSN:
Container-title:56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Ting Eric¹,Nguyen Nhan T.²,Lebofsky Sonia¹

Affiliation:

1. Stinger Ghaffarian Technologies, Inc.

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1407

Reference40 articles.

1. 0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 18 -0.1 0.0 -0.3 0.4 -1.1 2.1 -0.2 -1.1 2.6 -1.9 2.9 -2.1 0.6 -0.9 1.5 19 0.3 0.0 0.2 0.0 0.4 0.8 1.0 -2.4 4.7 -0.1 1.2 -1.2 -0.3 1.4 -0.1 20 0.7 0.1 0.3 0.4 -0.2 1.7 0.5 -0.9 3.4 0.4 1.1 -0.7 0.2 1.1 -0.8 21 0.0 0.1 0.2 -0.1 0.2 0.1 -0.2 -0.7 3.4 -0.7 0.9 -0.5 0.6 0.4 1.2 22 0.5 -0.3 0.4 0.4 -0.6 0.7 -0.5 -0.1 2.2 -0.8 0.6 -0.1 1.6 -1.5 3.7 23 1.7 0.5 1.1 1.6 0.4 2.3 1.6 -1.0 5.4 2.4 0.2 2.2 2.7 -1.6 3.8 24 1.9 0.6 1.2 1.9 0.1 3.3 2.5 -1.2 5.0 2.1 1.8 0.1 1.7 -0.7 4.1 69 0.3 0.2 -0.5 0.7 -0.7 0.8 0.4 -0.4 1.1 -0.6 1.1 -0.9 1.3 -0.8 -1.5 70 1.0 0.0 0.9 0.7 0.8 0.4 1.0 -1.2 3.9 0.0 1.8 -0.9 1.7 -2.1 1.7 71 1.5 0.5 0.7 1.7 0.3 1.7 1.2 0.6 1.5 1.4 0.6 1.4 1.5 0.3 -0.3

2. 2.2 0.9 0.6 3.0 0.0 2.6 1.8 1.7 0.4 2.8 1.4 0.5 2.1 -0.8 1.8 Mean 0.91 0.24 0.44 0.97 -0.04 1.50 0.83 -0.61 3.05 0.45 1.23 -0.20 1.25 -0.47 1.37

3. 0 2.0 10.0 4.0 5.0 4.0 5.0 3.0 4.0 4.0 6.0 5.0 5.0 10.0 10.0 32 0.2 2.6 8.2 1.5 1.4 9.2 0.3 2.8 5.4 -0.3 4.6 6.3 -0.1 4.3 807 33 0.2 2.5 8.9 0.9 2.7 6.9 2.1 1.2 6.6 0.6 3.2 7.7 -1.2 6.9 4.6 34 1.4 2.6 9.0 3.0 1.6 9.7 3.6 1.2 7.8 5.4 -0.3 12.2 1.7 2.5 10.4 35 0.8 2.4 9.5 2.4 1.9 8.3 1.7 2.6 6.3 4.5 0.1 11.0 0.0 4.3 8.8

4. 2.0 2.4 9.8 2.8 2.9 8.5 4.3 0.8 8.6 9.8 -4.4 16.4 0.5 4.1 9.0 Mean 0.92 2.50 9.08 2.12 2.10 8.52 2.40 1.72 6.94 4.00 0.64 10.72 0.18 4.42 8.3

5. 0 3.0 5.0 5.0 6.0 5.0 6.0 6.0 11.0 5.0 6.0 5.0 4.0 6.0 5.0 37 0.6 3.0 4.1 2.5 2.7 9.9 2.5 5.4 13.8 3.4 3.6 9.6 1.2 0.8 6.2 38 1.0 2.8 1.0 2.8 1.7 11.1 2.4 5.2 14.6 3.2 2.6 9.7 0.6 1.8 3.1 39 0.9 2.6 4.7 2.2 2.8 9.8 3.5 4.1 14.9 5.0 1.0 11.9 1.8 -0.4 7.9 40 1.5 2.4 5.3 2.8 3.1 9.5 2.4 5.6 14.3 7.3 0.0 13.3 1.1 0.9 5.6

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