Natural Laminar Flow Design of a Supersonic Transport Jet Wing Body-Reference-Cited by-同舟云学术

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Natural Laminar Flow Design of a Supersonic Transport Jet Wing Body

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Iuliano Emiliano¹,Salah El Din Itham²,Donelli Raffaele¹,Quagliarella Domenico¹,Arnal Daniel²

Affiliation:

1. CIRA

2. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1279

Reference56 articles.

1. 1Arnal, D. “Boundary Layer Transition: Predictions Based on Linear Theory,” Tech. Rep. 793, AGARD, 1994.

2. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition

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. Attenuation of boundary-layer instabilities for natural laminar flow design on supersonic highly swept wings;Chinese Journal of Aeronautics;2024-07

2. Supersonic Natural Laminar Flow Effect on Axisymmetric Bodies with Sinusoidal Deformation;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2014

3. A Gradient-based Optimization Method for Natural Laminar Flow Design;Seventh IUTAM Symposium on Laminar-Turbulent Transition;2009-11-10

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