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Heat-requirements for ice protection of a cyclically gas-heated, 36 degree swept airfoil with partial-span leading-edge slat

机译：具有部分跨度前缘缝翼的循环气体加热36度后掠翼型的防冰需求

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Gray, Vernon H; Von Glahn, Uwe H;
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年度 1956
页码 1-74
总页数 74
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Cyclicity of Peru-Chile trench sediments between 36 degrees and 38 degrees S: A footprint of paleoclimatic variations? [J] . Rauch K Geophysical Research Letters . 2005,第8期

机译：秘鲁-智利海沟沉积物在36度和38度之间的周期性：古气候变化的足迹？
2. Autonomous Leading-Edge Slat Device for Reduction of Aeroacoustic Noise Associated with Aircraft Wings [J] . NASA Tech Briefs . 2016,第5期

机译：自主的前沿板条装置，用于减少与飞机机翼相关的航空声噪声
3. Leading-edge vortices over swept-back wings with varying sweep geometries [J] . William B. Lambert, Mathew J. Stanek, Roi Gurka, Royal Society Open Science . 2019,第7期

机译：后掠翼上的前缘涡流具有不同的掠掠几何形状
4. Method of Calculating Flow around Extremely Thin Airfoil with Slotted Leading-edge Slat and Flap [C] . Vladimir A. Frolov Conference on High-Energy Processes in Condensed Matter . 2019

机译：用开槽前缘板条和翼片绕极薄翼型计算流动的方法
5. Aerodynamic effects of simulated ice shapes on two-dimensional airfoils and a swept finite tail. [D] . Alansatan, Sait. 2001

机译：模拟冰形状对二维机翼和扫掠有限尾翼的空气动力学影响。
6. Leading-edge vortices over swept-back wings with varying sweep geometries [O] . William B. Lambert, Mathew J. Stanek, Roi Gurka, 2019

机译：后掠翼上的前缘涡旋具有不同的掠掠几何形状
7. Modeling intermittent leading-edge vortex shedding in unsteady airfoil flows with reduced-count discrete vortices [O] . Ramesh Kiran, Suresh Babu Arun Vishn, Gopalarathnam Ashok 2015

机译：在不稳定翼型流中建模间歇前缘涡旋脱落，减少计数离散涡旋

Heat-requirements for ice protection of a cyclically gas-heated, 36 degree swept airfoil with partial-span leading-edge slat

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