Static Nonlinear Aeroelastic Analysis of a Blended Wing Body

Author:

Beran Philip1,Hur JiYoung2,Snyder Richard1,Strong Daniel1,Bryson Dean1,Strganac Thomas3

Affiliation:

1. Air Force Research Laboratory

2. Mississippi State University

3. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

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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1. An efficient method for nonlinear flutter of the flexible wing with a high aspect ratio;Aerospace Systems;2018-06

2. Accelerated loosely-coupled CFD/CSD method for nonlinear static aeroelasticity analysis;Aerospace Science and Technology;2010-06

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

4. The SensorCraft Configurations: A Non-Linear AeroServoElastic Challenge for Aviation;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18

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