Stability Analysis of Full Geometry Aircraft through CFD and Response Surface Method
Author:
Affiliation:
1. Konkuk University
2. Kon-kuk University,
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1434
Reference15 articles.
1. Nicolai,LelandM,fundamentalofaircraftdesign,METS,INC,Xenia,OH,1975.
2. Influence of support oscillation in dynamic stability tests
3. Nelson,R.C.,FlightStabilityandAutomaticControl,2ndedition,McGraw-Hill,NewYork,NY1998.
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