REU Site: Advanced Technologies for HYpersonic, Propulsive, Energetic, and Reusable Platforms (HYPER)

REU 网站：超音速、推进、充满活力和可重复使用平台的先进技术 (HYPER)

• 批准号: 1852130
• 负责人: Ali Gordon
• 金额: $ 38.24万
• 依托单位: The University of Central Florida Board of Trustees
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 2019
• 资助国家: 美国
• 起止时间: 2019-03-15 至 2023-02-28
• 项目状态: 已结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=1852130&HistoricalAwards=false
• 关键词: REU; Site; Advanced; Technologies; HYpersonic

The Research Experience for Undergraduates (REU) Site: Advanced Technologies for Hypersonic, Propulsive, Energetic and Reusable Platforms (HYPER) at the University of Central Florida (UCF) addresses challenges in next-generation modes of transportation and energy generation. Realizing planned platforms for advanced space travel and energy production can only be achieved through multidisciplinary research. This REU site will actively recruit and partner a diverse group of approximately 33 students over 3 years with leading faculty and graduate students at UCF. Together, these teams will advance the fundamental knowledge needed to overcome technical barriers limiting hypersonic flight. Candidate REU students will be matched with individual research projects based on their interests and skills. With the majority of their time engaged in cutting-edge research, REU students will also benefit from research-oriented seminars, professional development workshops, software training, and launch pad facility tours. HYPER has several goals; most importantly, to prepare students for PhD-level research and research-oriented employment.HYPER will cultivate and unite multidisciplinary interests to study advanced structures and systems with application to hypersonics, space, propulsion, and energy. For example, components in launch vehicles are subjected to combined extreme environments where fluid-structure interactions are key considerations. Also, advanced manufacturing must be better understood to improve component performance and reduce weight. Frameworks for modeling digital versions of systems must be created to predict overall performance more accurately. Participants will gain hands-on research training in contemporary challenges such as: (1) utilizing advanced manufacturing techniques for high-value components, (2) integrating in situ monitoring of stress- strain evolution, (3) developing novel methods for improved internal cooling and heat transfer effectiveness, (4) mitigating flutter through advanced rotor dynamic control, etc. Eleven modules are crafted to engage students in PhD-level topics; these research topics rely on approaches that cut across disciplines and techniques (e.g., experiments and simulations). As a result, HYPER will play a key role in preparing a workforce of young engineers and scientists for research careers in these areas.This site is supported by the Department of Defense in partnership with the NSF REU program.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

本科生研究体验 (REU) 网站：中佛罗里达大学 (UCF) 的高超音速、推进、能量和可重复使用平台先进技术 (HYPER) 解决了下一代运输和能源生成模式的挑战。实现先进太空旅行和能源生产的计划平台只能通过多学科研究来实现。该 REU 站点将在 3 年内积极招募大约 33 名学生组成的多元化群体，并与 UCF 的顶尖教师和研究生合作。这些团队将共同推进克服限制高超音速飞行的技术障碍所需的基础知识。 REU 候选学生将根据他们的兴趣和技能与个人研究项目相匹配。由于 REU 学生的大部分时间都从事前沿研究，因此他们还将受益于研究型研讨会、专业发展研讨会、软件培训和发射台设施参观。 HYPER 有几个目标；最重要的是，为学生进行博士级研究和研究型就业做好准备。HYPER 将培养和联合多学科兴趣，研究应用于高超音速、空间、推进和能源的先进结构和系统。例如，运载火箭中的部件要承受极端的综合环境，其中流体-结构相互作用是关键考虑因素。此外，必须更好地理解先进制造，以提高部件性能并减轻重量。必须创建用于系统数字版本建模的框架，以更准确地预测整体性能。参与者将获得针对当代挑战的实践研究培训，例如：(1) 利用先进制造技术生产高价值部件，(2) 集成应力应变演变的现场监测，(3) 开发改进内部冷却的新方法和传热效率，（4）通过先进的转子动态控制减轻颤振等。精心设计了十一个模块来吸引学生参与博士级别的主题；这些研究主题依赖于跨学科和技术的方法（例如实验和模拟）。因此，HYPER 将在为这些领域的研究职业培养年轻工程师和科学家队伍方面发挥关键作用。该网站由国防部与 NSF REU 计划合作支持。该奖项反映了 NSF 的法定使命和通过使用基金会的智力优点和更广泛的影响审查标准进行评估，该项目被认为值得支持。

项目成果

Undergraduate Hypersonics Research: Lessons From Two Years of the REU Site HYPER

本科生高超音速研究：REU 站点 HYPER 两年的经验教训

• DOI: 10.1115/gt2022-81021
• 发表时间: 2022
• 期刊: ASME Turbo Expo 2022
• 作者: Kauffman, Jeffrey L.;Gordon, Ali P.
• 通讯作者: Gordon, Ali P.

Development of an Automatic-Calibrating Small-Scale Thrust Stand for Rotating Detonation Rocket Engines

旋转爆震火箭发动机自动标定小型推力台的研制

• DOI: 10.2514/6.2022-2370
• 发表时间: 2022
• 期刊: AIAA SciTech 2022 Forum
• 作者: Burke, Robert F.;Rezzag, Taha;Rodriguez, Alexander;Garcia, Kian;Ahmed, Kareem A.;Kotler, Adam
• 通讯作者: Kotler, Adam

Analysis of Rocket Jet Particulate using Euler-Lagrange and Euler-Euler Approaches

• DOI: 10.2514/6.2020-1797
• 发表时间: 2020-01
• 作者: D. Fontes;D. Mikkelsen;M. Kinzel

Undergraduate Hypersonics Research: The First Year of the REU Site HYPER

本科生高超音速研究：REU 站点 HYPER 的第一年

• DOI: 10.2514/6.2021-0354
• 发表时间: 2021
• 期刊: AIAA SciTech 2021
• 作者: Kauffman, Jeffrey L.;Gordon, Ali P.
• 通讯作者: Gordon, Ali P.

Dynamic Mode Decomposition Study of a RDRE Exhaust for Swirl Attenuation Using Various Nozzle Configurations

使用各种喷嘴配置进行涡流衰减的 RDRE 排气的动态模式分解研究

• DOI: 10.2514/6.2022-0516
• 发表时间: 2022
• 期刊: AIAA SciTech 2022 Forum
• 作者: Rezzag, Taha;Burke, Robert F.;Rodriguez, Alexander;Garcia, Kian;Stiehl, Bernhard;Ahmed, Kareem A.
• 通讯作者: Ahmed, Kareem A.