Optimization of Variable-Camber Continuous Trailing-Edge Flap Configuration for Drag Reduction
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. MORI Associates, Moffett Field, California 94035
3. University of Washington, Seattle, Washington 98195
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034810
Reference59 articles.
1. Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development
2. Development of Mission Adaptive Digital Composite Aerostructure Technologies (MADCAT)
3. Aerodynamic Flight Test Results for the Adaptive Compliant Trailing Edge
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