Forced Oscillation Wind Tunnel Testing for FASER Flight Research Aircraft
Author:
Affiliation:
1. The Boeing Company
2. NASA Langley Research Center
3. Massachusetts Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4645
Reference9 articles.
1. Global Modeling of Pitch Damping from Flight Data
2. 4Garza, F.R. and Morelli, E.A. "A Collection of Nonlinear Aircraft Simulations in MATLAB®," NASA TM-2003-212145, January2003.
3. Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER Project
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