Numerical Analysis of Static and Dynamic Performances of Grid Fin Controlled Missiles
Author:
Affiliation:
1. Royal Military College of Canada, Kingston, Ontario K7K 7B4, Canada
2. Defence Research and Development Canada, Quebec City, Québec G3J 1X5, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33189
Reference39 articles.
1. A comprehensive CFD investigation of grid fins as efficient control surface devices
2. Viscous CFD calculations of grid fin missile aerodynamics in the supersonic flow regime
3. Analysis of Grid Fins for Launch Abort Vehicle Using a Cartesian Euler Solver
4. Grid Fin Stabilization of the Orion Launch Abort Vehicle
Cited by 16 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. An Efficient Method to Determine the Dynamic Stability of a Missile/Rocket Configuration with Grid Fins;2024
2. Application of Perforated Stabilizers for Static Stability at Subsonic Flight Speeds of the Separation Unit of a Spacecraft Emergency Escape System;Russian Aeronautics;2022-10
3. Numerical Investigation of Aeroelastic Characteristics of Grid Fin;AIAA Journal;2021-12-22
4. Validity of the Concept of the Unit Grid Fin by 3-D Calculation of Supersonic Grid Fin Flows;Journal of the Korean Society for Aeronautical & Space Sciences;2021-08-31
5. Aerodynamics Analysis of Grid Fins Inner Lattice Structure in Cruise Missile;WSEAS TRANSACTIONS ON FLUID MECHANICS;2021-05-19
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3