Wind Tunnel Test of a Three-Element Airfoil Configuration: Development of Experimental Apparatus and Procedure for Obtaining Reliable Results

Author:

Girardi Roberto1,Assato Marcelo1,Fico Nide1,Komatsu Paulo2

Affiliation:

1. Technological Institute of Aeronautics

2. EMBRAER

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. 2Elsenaar,A."Wallblowingrequirements for2-Dhigh lift testing in pessurizedwind tunnels", National Aerospace Laboratory,NLR,The Netherlands,NLR Memorandum AC 83-005U",1983.

2. 4Girardi, R.M.; Fico Jr, N.G.C.R; Mello, O.A.F; Komatsu, P. "Research Wind Tunnel of the Aeronautical Institute ofTechnology:ManufactoringAspectsand Design Details".In:COBEM2003,SãoPaulo,2003.

3. Calibration of a Boundary-Layer Control System for Use in a Low-Speed Wind Tunnel

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