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Increase of Critical Mach Number by Local Linearization Method and Airfoil Construction at Subsonic and Transonic Regimes

机译：亚态和跨音质制度的局部线性化方法和翼型施工的临界机械数量增加

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Ali. S. Bazgir; Sergey. A. Takovitskii;
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1. Increase of Critical Mach Number by Local Linearization Method and Airfoil Construction at Subsonic and Transonic Regimes [J] . Bazgir Ali. S., Takovitskii Sergey. A. MATEC Web of Conferences . 2018,第期

机译：亚态和跨音质制度的局部线性化方法和翼型施工的临界机械数量增加
2. Scalable gradient-enhanced artificial neural networks for airfoil shape design in the subsonic and transonic regimes [J] . Bouhlel Mohamed Amine, He Sicheng, Martins Joaquim R. R. A. Structural and multidisciplinary optimization . 2020,第4期

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3. The flow separation development analysis in subsonic and transonic flow regime of the laminar airfoil [J] . Robert Placek, Pawe? Rucha?a Transportation Research Procedia . 2018,第1期

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4. Hot-wire Calibration at High Subsonic Transonic Mach Numbers [C] . J. H. Watmuff, M.B.Jones, S. M. Henbest, Australasian fluid mechanics conference . 2012

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5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

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8. TRANSONIC-WING INVESTIGATION IN THE LANGLEY 8-FOOT HIGH-SPEED TUNNEL AT HIGH SUBSONIC MACH NUMBERS AND AT A MACH NUMBER OF 1.2 ANALYSIS OF PRESSURE DISTRIBUTION OF WING-FUSELAGE CONFIGURATION HAVING A WING OF 45° SWEEPBACK, ASPECT RATIO 4, TAPER RATIO 0.6, AND- NACA 65A006 AIRFOIL SECTION [R] . Donald L. Loving, Bruce B. Estabrooks 1951

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Increase of Critical Mach Number by Local Linearization Method and Airfoil Construction at Subsonic and Transonic Regimes

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