Part 2: Preparation for Wind Tunnel Model Testing and Verification of Cal Poly's AMELIA 10 Foot Span Hybrid Wing-Body Low Noise CESTOL Aircraft
Author:
Affiliation:
1. California Polytechnic State University
2. Georgia Tech Research Institute
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1307
Reference15 articles.
1. 1Marshall,D.,Jameson,K.,Golden,R.,Welborn,A.,Erhmann,R."NRAFinalYearOneReport,"NASANRA,2008.
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1. STOL Performance of Cal Poly's AMELIA;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
2. Summary of the Aerodynamic Modeling Efforts for AMELIA;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
3. Acoustic Surveys of a Scaled-Model CESTOL Transport Aircraft in Static and Forward Speed Conditions;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
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