Numerical study of the injection process in a transonic wind tunnel: The numerical details

Author:

Falcão Filho João B.P.,Ortega Marcos A.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference38 articles.

1. Bedrzhitsky EI, Roukavets VP. Historical review of the creation and improvement of aerodynamic test facilities at TsAGI. In: AGARD conference proceedings 585, Article 1, Moscow; 1997.

2. Carrière P. The injector driven tunnel. In: Proceedings of the von Kàrmàn institute for fluid dynamics, Lecture series on large transonic wind tunnels, von Kármán Institute for Fluid Dynamics, Brussels, Belgium; 1973.

3. Arkadov YK, Roukavets VP. Ejector-driven wind tunnels. In: AGARD conference proceedings 585, Article 22, Moscow; 1997.

4. Muhlstein Jr L, Petroff DN, Jillie DW. Experimental evaluation of an injector system for powering a high Reynolds number transonic facility. AIAA Paper 74-632; 1974.

5. Prediction of transients and control reactions in a transonic wind tunnel;Falcão;J Braz Soc Mech Eng Sci,2000

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1. The Mach number prediction based on the feature subsets ensemble in transonic wind tunnel;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2015-12-22

2. Ensemble Fixed-Size LS-SVMs Applied for the Mach Number Prediction in Transonic Wind Tunnel;IEEE T AERO ELEC SYS;2015

3. Numerical Study of Wall Ventilation in a Transonic Wind Tunnel;Journal of Aerospace Technology and Management;2015-02-22

4. A Numerical and Experimental Study of an Airfoil in a Transonic Wind Tunnel;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

5. Numerical study of the injection process in a transonic wind tunnel. Part II: The off-design points;Computers & Fluids;2009-04

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