48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2010
DOI: 10.2514/6.2010-1309
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Model-Based Predictive Control System in a Transonic Aerodynamic Test Facility

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“…(8) and (9), k i are the total pressure loss factors in the n sections of the wind tunnel defined by the mechanical energy or "head loss" equation:…”
Section: Mathematical Modelmentioning
confidence: 99%
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“…(8) and (9), k i are the total pressure loss factors in the n sections of the wind tunnel defined by the mechanical energy or "head loss" equation:…”
Section: Mathematical Modelmentioning
confidence: 99%
“…M ATHEMATICAL models for the behavior of wind tunnels and test facilities have been developed for a variety of reasons [1][2][3][4][5][6][7][8]. For example, in [1], a mathematical model of a new wind tunnel was developed to ensure that the facility would achieve its target test envelope.…”
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confidence: 99%
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