The design and installation of a turbulence reduction system for the NASA Ames 11- by 11-foot Transonic Wind Tunnel

Author:

Murthy Sreedhara1,Kmak Frank2,Koss Brian2

Affiliation:

1. Calspan Corp., Moffett Field, CA

2. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

Cited by 5 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. Flow Angularity Investigations in an Automotive Slotted Wall Wind Tunnel;Energies;2019-11-30

2. Wake Effects of Honeycomb Stiffeners;24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2004-06-19

3. Revalidation of the NASA Ames 11-by 11-foot transonic wind tunnel with a commercial airplane model;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

4. Flow quality measurements in the NASA Ames upgraded 11-by 11-foot transonic wind tunnel;21st Aerodynamic Measurement Technology and Ground Testing Conference;2000-06-19

5. Modernization and activation of the NASA Ames 11- by 11-Foot Transonic Wind Tunnel;21st Aerodynamic Measurement Technology and Ground Testing Conference;2000-06-19

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