Analysis of Stall Aerodynamics of a Swept Wing with Laminar-Flow Glove
Author:
Affiliation:
1. Aerodynamics and Propulsion Branch, NASA Armstrong Flight Research Center, Edwards, California 93523
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032883
Reference6 articles.
1. A Transonic Laminar-Flow Wing Glove Flight Experiment: Overview and Design Optimization
2. Laminar Flow Control on a Swept Wing with Distributed Roughness
3. Analysis of Asymmetric Aircraft Aerodynamics Due to an Experimental Wing Glove
4. Summary of the First AIAA CFD High-Lift Prediction Workshop
5. Overview of the 1st AIAA CFD High Lift Prediction Workshop
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2. Computational Fluid Dynamics Analysis of the Stall Characteristics of a Wing Designed Based on Prandtl’s Minimum Induced Drag;2018 Applied Aerodynamics Conference;2018-06-24
3. Longitudinal Aerodynamic Modeling of the Adaptive Compliant Trailing Edge Flaps on a GIII Aircraft and Comparisons to Flight Data;AIAA Atmospheric Flight Mechanics Conference;2016-06-10
4. Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Seamless Flaps;34th AIAA Applied Aerodynamics Conference;2016-06-10
5. Efficient stall compliance prediction method for trimmed very light aircraft with high-lift devices;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-05-16
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