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Pounds per square inch Active Aeroelastic Wing Acrylonitrile Butadiene Styrene Air Force Test and Evaluation Center Air Force Wright Laboratory Angle of Attack Computer Numerical Control Defense Advanced Research Projects Agency Fused Deposition Modeling Langley Research Center Mission Adaptive Wing National Advisory Committee for Aeronautics The document describes the design and analysis of a multi-section variable camber wing. The wing model has six sections that can each rotate up to 5 degrees, changin
- Author
- Nagaraj Ramachandrappa
- Language
- EN