Experimental Study of the Turbulence Level at the Intake of an Open Circuit Wind Tunnel

Author:

Assato Marcelo1,Fico Nide1,Girardi Roberto1

Affiliation:

1. Instituto Tecnológico de Aeronáutica

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Barlow, J.B., Rae. W. H. Jr. and Pope, A., 1999, Low Speed Wind Tunnel Testing,John&Sons,ThirdEdition,Inc.

2. Kline, S.J. and McClintock, F. A., 1953, Describing Uncertainties in Single-Sample Experiments, JournalMechanical Engineering.

3. Manuel. G. S., Molloy, J.K. and Barna, P. S. "Effect of the Collector Configuration on Test Section Turbulence Levels in an Open-Jet Tunnel,"NASA TM-4333.

4. McKinney, M. and Scheiman, J., 1981, Evaluation of Turbulence Reducing Devices for the Langley 8 foot Transonic PressureTunnel",NASA TM81792.

5. Comprehensive Design of Axisymmetric Wind Tunnel Contractions

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. Air Intake Influence on the Test-section Flow Quality of an Open-Circuit Wind Tunnel;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

2. Research Wind Tunnel of the Aeronautical Institute of Technology: Conceptual Design and Calibration;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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