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Laminar-turbulent transition in the vicinity of blunt leading edge of flat delta wing in hypersonic flow

机译：层间湍流过渡在高超声道中平三角翼的钝器前缘附近

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A. V. Vaganov; D. V. Grachikov; V. M. Kashin; V. D. Nemykin; A. Yu. Noev; V. N. Radchenko; A. S. Skuratov; V. I. Shalaev;
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1. Correlation of laminar-turbulent transition data over flat plates in supersonic/hypersonic flow including leading edge bluntness effects [J] . Simeonides GA. Shock Waves . 2003,第6期

机译：超音速/人身流动中平板层流湍流转换数据的相关性，包括前沿钝化效应
2. INFLUENCE OF THE PLATE LEADING-EDGE SHAPE AND THICKNESS ON THE BOUNDARY LAYER LAMINAR-TURBULENT TRANSITION IN HYPERSONIC FLOW [J] . S.V. Aleksandrov, E.A. Aleksandrova, V.Ya. Borovoy, TsAGI science journal . 2019,第5期

机译：板缘边缘形状和厚度对高辐射流动边界层层状湍流过渡的影响
3. Distinctive Features of Flow in the Hypersonic Boundary Layer in the Vicinity of the Plane of Symmetry of a Planar Wing Having a Bend of the Leading Edge [J] . Dudin G. N., Ledovskii A. V. Fluid Dynamics . 2019,第4期

机译：在具有前缘弯曲的平面翼的对称平面附近的高超声边界层流动的独特特征
4. Laminar-turbulent transition in the vicinity of blunt leading edge of flat delta wing in hypersonic flow [C] . A. V. Vaganov, D. V. Grachikov, V. M. Kashin, Conference on High-Energy Processes in Condensed Matter . 2017

机译：层间湍流过渡在高超声道中平三角翼的钝器前缘附近
5. THE LIFT ON DELTA WINGS WITH LEADING EDGE SEPARATION IN PERIODIC FLOW. [D] . STEPHENS, ALTON LEE, JR. 1970

机译：三角翼上的举升装置具有周期性流动中的前缘分离功能。
6. The leading-edge vortex of swift wing-shaped delta wings [O] . Rowan Eveline Muir, Abel Arredondo-Galeana, Ignazio Maria Viola 2017

机译：快翼形三角翼的前沿旋涡
7. The Effects of Angle of Attack on Viscous Hypersonic Flowfield over a Flat Plate with a Slightly Blunt Leading Edge. [O] . Takeyoshi KIMURA, Hajime ITOH, Kazuhiko OGAWA 1996

机译：浅钝领导型粘粘性过度流场对粘性超声波流域的影响。

Laminar-turbulent transition in the vicinity of blunt leading edge of flat delta wing in hypersonic flow

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