Research Wind Tunnel of the Aeronautical Institute of Technology: Conceptual Design and Calibration

Author:

Assato Marcelo1,Girardi Roberto2,Fico Nide2,Mello Olympio3,Komatsu Paulo4

Affiliation:

1. Instituto Tecnológico de Aeonáutica

2. Instituto Tecnológico de Aeronáutica

3. Centro Técnico Aeroespacial

4. EMBRAER

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. • Assato, M, Fico Jr., N.G.C.R. and Girardi, R.M. 2003,Experimental Study of the Turbulence Level at the Intake an Open Circuit Wind Tunnel, AIAAPAPER2003-3848l

2. • Cochran, D.L. & Kline, S.J., 1958, "Use of Short Flat Vanes for Producing Efficient Wide-Angle Two-Dimensional SubsonicDiffusers",NACATN-4309.

3. • Eckert, W.T.; Mort, K.W. & Jope, J., 1976, "Aerodynamic Design Guidelines and Computer Program for Estimation of Subsonic Wind Tunnel Performance", NASA TN D-8243.

4. • Eckert, W.T.; Mort, K.W. & Piazza, J.E., 1976, "An Experimental Investigation of End Treatments for Nonreturn Wind Tunnels", NASA TMX-3402.

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