Adjoint Method and Predictive Control for 1-D Flow in NASA Ames 11-Foot Transonic Wind Tunnel-Reference-Cited by-同舟云学术

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Adjoint Method and Predictive Control for 1-D Flow in NASA Ames 11-Foot Transonic Wind Tunnel

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Nguyen Nhan¹,Ardema Mark²

Affiliation:

1. NASA Ames Research Center

2. Santa Clara University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1433

Reference11 articles.

1. Saunder, G. "UPWT Modernization Final Design Test Section Model Revision for the 11-Ft Tunnel Simulation",ContractNo. NAS2-13032,SverdrupTechnology,1991.

2. Hirsh,C.,NumericalComputationofInternalandExternalFlows, Vol. 1,JohnWiley&Sons,Brussels, 1991.

3. Optimal Control of Flow Recirculation in a Wind Tunnel

Cited by 2 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. Mach Number Control for Continuous Mode Tests in Wind Tunnel Using Feed Forward Algorithm;Lecture Notes in Electrical Engineering;2019

2. Mach Number Control improvement in ONERA S1MA large Transonic Wind Tunnel;30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2014-06-13

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