云南高校图书馆联盟文献共享服务平台- CANARD

CANARD: 作品数：35被引量：54H指数：4; 导出分析报告; 相关领域：航空宇航科学技术更多>>; 相关作者：李秀敏莫嘉琪张国庆杨树兴陈前更多>>; 相关机构：天津大学安徽师范大学上海交通大学北京理工大学更多>>; 相关期刊：《Journal of Beijing Institute of Technology》《今日中国（法文版）》《Transactions of Nanjing University of Aeronautics and Astronautics》《明日风尚》更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划中国科学院知识创新工程重要方向项目上海市教委E研究院-上海高校网格项目更多>>

The influence of roll angles on unsteady aerodynamics in a canard-configured missile: 《International Journal of Mechanical System Dynamics》2024年第2期213-225,共13页Kai Wei Shaosong Chen Dongdong Tang Yihang Xu Xujian Lyu Qing Chen; Fund of Science and Technology on Underwater Information and Control Laboratory,Grant/Award Number:2021-JCJQ-LB-030-05。; During the initial stage of vertical launch,a missile may exhibit an uncertain roll angle(φ)and a high angle of attack(α).This study focuses on examining the impact of roll angle variations on the flow field and the...; 关键词：large angle of attack roll angle unsteady separated flow power spectral density proper orthogonal decomposition

Canards Flying on Bifurcation: 《Advances in Pure Mathematics》2023年第6期412-424,共13页Shuya Kanagawa Kiyoyuki Tchizawa; There exists a property “structural stability” for “4-dimensional canards” which is a singular-limit solution in a slow-fast system with a bifurcation parameter. It means that the system includes the possibility t...; 关键词：Canard Solution Slow-Fast System Nonstandard Analysis Hilbert’s 16th Problem Brownian Motion Stochastic Differential Equation

Effect of longitudinal lift distribution on sonic boom of a canard-wing-stabilator-body configuration被引量：1: 《Chinese Journal of Aeronautics》2023年第6期92-108,共17页Liwen ZHANG Zhonghua HAN Jianling QIAO Wenping SONG Yulin DING Xuehe WANG; sponsored by the National Natural Science Foundation of China(Nos.12072285,U20B2007);the Shaanxi Science Fund for Distinguished Young Scholars,China(No.2020JC-13);the Natural Science Funding of Shaanxi Province,China(No.2020JM-127).; After the last flight of the Concorde in 2003,sonic boom has been one of the obstacles to the return of a supersonic transport aircraft to service.To reduce the sonic boom intensity to an acceptable level,it is of gre...; 关键词：Computational fluid dynamics Longitudinal lift distribution Sonic boom Sonic boom reduction Supersonic transport

Structural Stability in 4-Dimensional Canards: 《Advances in Pure Mathematics》2022年第11期600-613,共14页Shuya Kanagawa Kiyoyuki Tchizawa; Let us consider higher dimensional canards in a sow-fast system R²⁺² with a bifurcation parameter. Then, the slow manifold sometimes shows various aspects due to the bifurcation. Introducing a key notion “...; 关键词：Canard Solution Slow-Fast System Nonstandard Analysis Hilbert’s 16th Problem Brownian Motion Stochastic Differential Equation

Canard Solutions in a Predator-Prey Model: 《Journal of Applied Mathematics and Physics》2022年第5期1678-1693,共16页Guojian Lin; The canard explosion phenomenon in a predator-prey model with Michaelis-Menten functional response is analyzed in this paper by employing the geometric singular perturbation theory. First, some turning points, such as...; 关键词：Canard Explosion Relaxation Oscillation Predator-Prey Model Geometric Singular Perturbation Theory

Canard explosion,homoclinic and heteroclinic orbits in singularly perturbed generalist predator-prey systems: 《International Journal of Biomathematics》2021年第1期151-174,共24页Ali Atabaigi; This paper studies the dynamics of the generalist predator–prey systems modeled in[E.Alexandra,F.Lutscher and G.Seo,Bistability and limit cycles in generalist predator–prey dynamics,Ecol.Complex.14(2013)48–55].When...; 关键词：Canard cycle relaxation oscillation generalist predator prey singular perturbation HOMOCLINIC HETEROCLINIC

纸飞机工坊⑦滑翔性能优秀的纸飞机“Canard”: 《航空模型》2020年第7期36-37,共2页天上十年(文/图); 纸飞机发展简史(上)因历史久远,世界上第一架纸飞机已无法考证其具体的样式和性能。但可以确定的是,纸飞机是许多航空先驱设计飞机的起点:莱昂纳多·达·芬奇曾用羊皮纸制作纸飞机,以验证其设计的扑翼机;乔治·凯利在19世纪曾用纸飞机...; 关键词：发展简史扑翼机羊皮纸达·芬奇

A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails被引量：1: 《Journal of Harbin Institute of Technology(New Series)》2019年第6期62-68,共7页Ping’an Liu Mingyuan Liu; Sponsored by the Fundamental Research Funds for the Central Universities(Grant No.HEUCFG201815); The steady flow field of a canard missile on different angles of attack and Mach numbers were studied. Based on analysis, a method was proposed to reduce the calculation for the rolling characteristics of the canard m...; 关键词：numerical simulation canard missile free-spinning tail wind tunnel test rolling characteristics

Flight dynamics characteristics of canard rotor/wing aircraft in helicopter flight mode被引量：4: 《Chinese Journal of Aeronautics》2019年第7期1577-1587,共11页Honggang GAO Ao HE Zhenghong GAO Yang NA Yangping DENG; The aerodynamic layout of the Canard Rotor/Wing(CRW) aircraft in helicopter flight mode differs significantly from that of conventional helicopters. In order to study the flight dynamics characteristics of CRW aircraf...; 关键词：CANARD rotor/wing AIRCRAFT DYNAMICS analysis FLIGHT DYNAMICS HELICOPTER LINEARIZATION Model building

Roto-Stabilizer for Superb Pitch-Related Post-Stall Maneuvers and STOL被引量：1: 《Advances in Aerospace Science and Technology》2018年第3期61-70,共10页Chung-Kiak Poh Chung-How Poh; Stabilizers and their control surfaces are vital components in maneuvering an airplane during flight. However, a shortcoming of stabilizers is that they require airstream or propeller wash for them to work properly. I...; 关键词：Roto-Stabilizers Roto-Canard Aerobatics STOL TROPICAL CYCLONE

CANARD