January 05, 2013 conference-paper Open access A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft AIAA Aerospace Sciences Meeting DOI: 10.2514/6.2013-214 Full text (OA) OpenAlex Authors 0 Author list not loaded yet. Cited by 2 stored of 138 Search Sort Most cited Newest Oldest Patent citations Title Any typearticle review book-chapter conference-paper preprint dissertation book dataset other Any fieldAgricultural and Biological Sciences Arts and Humanities Biochemistry, Genetics and Molecular Biology Business, Management and Accounting Chemical Engineering Chemistry Computer Science Decision Sciences Dentistry Earth and Planetary Sciences Economics, Econometrics and Finance Energy Engineering Environmental Science Health Professions Immunology and Microbiology Materials Science Mathematics Medicine Neuroscience Nursing Pharmacology, Toxicology and Pharmaceutics Physics and Astronomy Psychology Social Sciences Veterinary Open access Methodology for Evaluating a Distributed Variable-Camber Trailing-Edge System in Preliminary Aircraft Design 2024 Journal of Aircraft article Engineering Aeroelasticity and Vibration Control 1 citations Evaluation of a Distributed Variable-Camber Trailing-Edge Flap System at Preliminary Aircraft Design Stage 2022 AIAA AVIATION Forum conference-paper Environmental Science Advanced Aircraft Design and Technologies 1 citations 2 results References 0