Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing Sweep-Reference-Cited by-同舟云学术

Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing Sweep

Published:2006-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Grant Daniel¹,Abdulrahim Mujahid¹,Lind Rick¹

Affiliation:

1. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6505

Reference20 articles.

1. Area (cm2) -15 -30 66.17 14.68 1028.11 -10 -20 73.97 13.12 1003.45 -5 -10 78.81 12.38 976.25 0 0 80.39 11.84 947.11 5 10 78.61 11.62 916.68 10 20 73.61 11.69 885.66 15 30 65.72 12.13 854.76

2. state magnitude phase (deg) magnitude phase (deg) forward velocity 221.16 -94.22 157.19 62.51 angle of attack 1.42 -143.60 54.90 160.73

3. pitch rate 50.20 -101.72 417.45 225.57

4. pitch angle 35.31 -189.12 49.87 108.47 angle of sideslip 0.05 -99.04 0.25 216.15

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