Static Nonlinear Aeroelastic Analysis of a Blended Wing Body
Author:
Affiliation:
1. Air Force Research Laboratory
2. Mississippi State University
3. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1944
Reference23 articles.
1. MichaelSirak,"USAF'sSensorCraftTakesShape,"Jane'sDefenceWeekly,May14,2003.
2. MichaelSirak,"USAFTacklesChallengesofSensorCraft,"Jane'sDefenceWeekly,November3,2004.
3. Wakayama,S.,andKroo,I."TheChallengeandPromiseofBlended-Wing-BodyOptimization,"AIAA98-4736,1998.
4. Huttsell, L., Schuster, D., Volk, J., Giesing, J., and Love, M. "Evaluation of Computational Aeroelasticity Codes for Loads and Flutter,"AIAAPaper 2001-0569.
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3. Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04
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