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An integrated study of structures, aerodynamics and controls on the forward swept wing X-29A and the oblique wing research aircraft

机译：对前掠翼X-29a和斜翼研究飞机的结构，空气动力学和控制的综合研究

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The results of an integrated study of structures, aerodynamics, and controls using the STARS program on two advanced airplane configurations are presented. Results for the X-29A include finite element modeling, free vibration analyses, unsteady aerodynamic calculations, flutter/divergence analyses, and an aeroservoelastic controls analysis. Good correlation is shown between STARS results and various other verified results. The tasks performed on the Oblique Wing Research Aircraft include finite element modeling and free vibration analyses.

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作者
Dawson, Kenneth S.; Fortin, Paul E.;
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年度 1987
页码 1-128
总页数 128
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AIRCRAFT CONTROL; APPLICATIONS PROGRAMS (COMPUTERS); MATHEMATICAL MODELS; OBLIQUE WINGS; RESEARCH AIRCRAFT; STRUCTURAL ANALYSIS; X-29 AIRCRAFT; FINITE ELEMENT METHOD; FLUTTER; FREE VIBRATION; SERVOCONTROL; UNSTEADY AERODYNAMICS;

机译：空气动力学特征;飞机控制;应用程序（计算机）;数学模型; OBLIQUE WINGs;研究飞机;结构分析; X-29飞机;有限元法;扑;自由振动;伺服控制; UNsTEaDY aERODYNamICs;

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专利

1. Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations [J] . G. Q. Zhang, S. C. M. Yu, A. Chien, Journal of Aircraft . 2013,第2期

机译：卡纳德前掠机翼构型的空气动力学特性
2. FLOW STUDIES OF A FORWARD SWEPT WING FITTED WITH ACTIVE FLOW CONTROL [J] . N. Findanis, N. A. Ahmed Advances and Applications in Fluid Mechanics . 2014,第2期

机译：具有主动流控制的前掠翼的流动研究
3. The Twist-Bending Behavior of Forward Swept Wings: A Case Study of a Glass/Carbon Hybrid Composite Structure [J] . L. Blasi, F. Caputo, A. DAmore, Macromolecular symposia . 2007,第0期

机译：前掠机翼的扭曲弯曲行为：以玻璃/碳杂化复合结构为例
4. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft [C] . Moustaine Adegbindin, Nathan Love, Rakesh K.Kapania, AIAA aviation forum;AIAA/ISSMO multidisciplinary analysis and optimization conference . 2016

机译：前掠翼和混合翼机体的人工智能控制功率优化
5. Integrated aerodynamic and control system design of oblique wing aircraft. [D] . Morris, Stephen James. 1990

机译：斜翼飞机的空气动力学和控制系统集成设计。
6. Improvement of the aerodynamic performance by wing flexibility and elytra–hind wing interaction of a beetle during forward flight [O] . Tuyen Quang Le, Tien Van Truong, Soo Hyung Park, 2013

机译：甲虫在前飞过程中的机翼灵活性和鞘翅与后翅的相互作用改善了空气动力学性能
7. On the estimation of stability and control characteristics of a generalised forward swept wing aircraft [O] . Heydari F. 1986

机译：广义前掠翼飞机稳定性和控制特性的估计
8. Integrated Study of Structures, Aerodynamics and Controls on the Forward Swept Wing X-29A and the Oblique Wing Research Aircraft [R] . Dawson, K. S., Fortin, P. E. 1987

机译：前掠翼X-29a和斜翼研究飞机的结构，空气动力学和控制的综合研究

An integrated study of structures, aerodynamics and controls on the forward swept wing X-29A and the oblique wing research aircraft

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