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Measurement of flow boundary condition data and wing pressures in a wind tunnel test of a 45 deg swept wing

机译：在45度后掠翼的风洞试验中测量流动边界条件数据和机翼压力

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William P. Dwyer.

机译：威廉·德威尔

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Dwyer William P. (William Patrick);
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年度 1990
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原文格式 PDF
正文语种 eng
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入库时间 2022-08-20 21:11:15

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2. Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint Measurements [J] . Mark N. Glauser, William S. Saric, Keith L. Chapman, AIAA Journal . 2014,第2期

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3. Two Optical Techniques Appropriate for Visualizing the Steady／Unsteady Vortical Flow Past a Highly Swept Delta—Wing Equipped with Double Vortex—Flaps in Low and High Speed Wind—Tunnel [J] . GongNI, DingdingXIN, 等非线性科学与数值模拟通讯：英文版 . 1998,第003期

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4. FLEXIBILITY OF AN ORNITHOPTER WING TESTED IN A WIND TUNNEL FLEXIBILITY OF AN ORITHOPTER WING TESTED IN A WIND TUNNEL [C] . M. B. Jones A. Valiyff, J. Harvey Congress of the International Council of the Aeronautical Sciences . 2012

机译：在风洞中测试的正鸟翅膀的灵活性在风洞中测试的正鸟翅膀的灵活性
5. Nonlinear stability and saturation of crossflow vortices in swept-wing boundary layers. [D] . Haynes, Timothy Scott. 1996

机译：后掠边界层中错流涡旋的非线性稳定性和饱和度。
6. Wind tunnel and numerical data on the ventilation performance of windcatcher with wing wall [O] . Payam Nejat, John Kaiser Calautit, Muhd Zaimi Abd. Majid, 2016

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7. Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50 [O] . Babister A. W. 1951

机译：具有后缘分裂式襟翼的后掠翼的压力分布测量：航空学院风洞工作总结1948-50

Measurement of flow boundary condition data and wing pressures in a wind tunnel test of a 45 deg swept wing

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