CFD Design and Flight Test of a Swept Laminar Flow Control Wing-Reference-Cited by-同舟云学术

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CFD Design and Flight Test of a Swept Laminar Flow Control Wing

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Carpenter Andrew¹,Solomon William¹,Sullivan Anne¹,Korntheuer Andrea J.¹,Harris Christopher¹

Affiliation:

1. Northrop Grumman Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3809

Reference16 articles.

1. Arnal D. 1994 Predictions based on linear theory. Progress in transition modeling, AGARD Rep. No. 709.

2. Stability of Three-Dimensional Boundary Layers

3. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

Cited by 3 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. Design and Characterization of High-Lift Capabilities for Slotted, Natural-Laminar-Flow Airfoils;Journal of Aircraft;2023-07

2. High-Lift Computational Strategy for Slotted, Natural-Laminar-Flow Airfoils;Journal of Aircraft;2021-11-22

3. High-Lift Simulations of Slotted, Natural-Laminar-Flow Airfoils;AIAA Scitech 2019 Forum;2019-01-06

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