Computational Investigation of Flow over Inflatable Airfoils at Multiple Reynolds Numbers
Author:
Affiliation:
1. Lafayette High School
2. Saint Louis University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-377
Reference20 articles.
1. Simpson, A., Jacob, J., Smith, S.Flight Control of a UAV with Inflatable Wings with Wing Warping,‖ AIAA Paper 2006-2831,24th AIAAAppliedAerodynamicsConference, San Francisco, California, June5-8,2006.
2. Jacob, J. and S.W. Smith,Design of HALE Aircraft Using Inflatable Wings,‖ AIAA Paper 2008-0167, 46thAIAA AerospaceScienceMeetingandExhibit,Reno, NV, January2008.
3. Santhanakrishnan, A., Jacob, J.Effect of Regular Surface Perturbations on Flow Over an Airfoil,‖ AIAA Paper 2005-5145,35th AIAAFluid DynamicsConference&Exhibit, Ontario,June6-92005.
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