Design and Integration of a Low Observable Intake for the MULDICON Platform
Author:
Affiliation:
1. Swedish Defense Research Agency (FOI)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3162
Reference15 articles.
1. Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation
2. Multi-Disciplinary Design and Performance Assessment of Effective, Agile NATO Air Vehicles
3. Conceptual Design of a 53deg Swept Flying Wing UCAV Configuration
4. Aerodynamic shaping design and vortical flow design aspects of a 53deg swept flying wing configuration
Cited by 7 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. Adjoint based aerodynamic shape optimization of a semi-submerged inlet duct and upstream inlet surface;Optimization and Engineering;2024-01-11
2. Acoustic Radiation from an Integrated High Aspect Ratio Rectangular Nozzle with Co-Flow;AIAA AVIATION 2023 Forum;2023-06-08
3. Numerical investigations on acoustic propagation effects for highly integrated intake ducts;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
4. A Novel Test Bed for the Aeroacoustic Investigation of UCAV Configurations with Highly Integrated Propulsion Systems;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
5. Numerical investigation of the unsteady distortion for an S-duct intake with mechanical vortex generators;International Journal of Heat and Fluid Flow;2022-06
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