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Collocation Flutter Analysis Study. Volume III (Continued): AICs - Computer Program to Calculate Unsteady Aerodynamic Influence Coefficients for Subsonic, Transonic and Supersonic Flight.

机译：搭配颤振分析研究。第三卷（续）：aICs - 计算亚音速，超音速和超音速飞行的非定常气动影响系数的计算机程序。

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作者
Ulbrich, D. R.;
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年度 1969
页码 1-324
总页数 324
原文格式 PDF
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Aerodynamic control surfaces; Computer programming; Flutter; Numerical analysis; Numerical integration; Stability; Supersonic characteristics; Transonic characteristics; Aerodynamic loading; Rectangular bodies; Sweptback wings; Guided missiles; Collocation(Mathematic;

机译：空气动力学控制面;计算机编程;颤振;数值分析;数值积分;稳定性;超音速特性;跨音速特性;气动载荷;矩形体;后掠翼;导弹;搭配（数学）;
入库时间 2022-08-29 11:42:09

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1. REVIEW OF THE GREEN＇S FUNCTION METHOD FOR STEADY ＆UNSTEADY，SUBSONIC，TRANSONIC ＆SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATIONS [J] . 中国航空学报：英文版 . 1995,第002期

机译：综述复杂配置周围稳定＆∞Unsteady，亚音速，跨音和抑制空气动力学的绿色功能方法
2. Influence of aerodynamic nonlinearity due to static panel-curvature on flutter of panels at transonic and low supersonic Mach numbers [J] . Bhatia Manav, Beran Philip Journal of Fluids and Structures . 2018,第期

机译：气体动力学非线性引起的静态面板曲率对跨音和低超声波马赫数的颤振
3. Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method [J] . Jeonghyun Cho, Cheolheui Han, Leesang Cho, International Journal for Numerical Methods in Fluids . 2003,第10期

机译：使用3D面板方法对亚音速，声速和超音速马赫数的机翼进行稳定/不稳定的空气动力学分析
4. Stochastic Variations in Aerodynamic Influence Coefficients (AICs): Effects on Flutter Prediction of a Generic Wing [C] . Prasun Bansal, Dale M. Pitt AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference . 2013

机译：空气动力学影响系数（AIC）的随机变化：对通用机翼颤振预测的影响
5. A computer program for the algebraic determination of control coefficients in Metabolic Control Analysis. [O] . S Thomas, D A Fell 1993

机译：用于在代谢控制分析中代数确定控制系数的计算机程序。
6. Fully unsteady subsonic and supersonic potential aerodynamics for complex aircraft configurations for flutter applications [O] . Tseng K., Morino L. 1975

机译：完全不稳定的亚音速和超音速潜在空气动力学，用于扑扑应用中的复杂飞机配置

Collocation Flutter Analysis Study. Volume III (Continued): AICs - Computer Program to Calculate Unsteady Aerodynamic Influence Coefficients for Subsonic, Transonic and Supersonic Flight.

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