Development of Advanced High Lift Leading Edge Technology for Laminar Flow Wings-Reference-Cited by-同舟云学术

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Development of Advanced High Lift Leading Edge Technology for Laminar Flow Wings

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Bright Michelle¹,Korntheuer Andrea¹,Komadina Steve¹,Lin John²

Affiliation:

1. Northrop Grumman Corporation

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-211

Reference9 articles.

1. Flow-Field Measurement of a Hybrid Wing Body Model with Blown Flaps

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. On the Use of Power-Based Parameters for Blowing Active Flow Control Systems;AIAA Journal;2023-03

2. High-lift design for a forward swept natural laminar flow wing;CEAS Aeronautical Journal;2019-05-11

3. Simulation of Laminar-Flow Compatible High-Lift Wing Configuration with Flow Control;Journal of Aircraft;2016-09

4. Unsteady Active Flow Control on the Leading Edge of a High-lift Configuration Thin Airfoil;8th AIAA Flow Control Conference;2016-06-10

5. Active Separation Control on the Morphed Leading Edge of a Thin Airfoil in High-Lift Configuration;8th AIAA Flow Control Conference;2016-06-10

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