发布求助
文献互助 智能选刊 最新文献

22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference最新文献

筛选
英文 中文
Correction: High temperature effects in conical nozzle flow 修正:高温影响锥形喷嘴流动
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5322.C1
B. Lima, J. F. A. Martos, I. Rêgo, D. R. Pinto, Felipe Jean da Costa
{"title":"Correction: High temperature effects in conical nozzle flow","authors":"B. Lima, J. F. A. Martos, I. Rêgo, D. R. Pinto, Felipe Jean da Costa","doi":"10.2514/6.2018-5322.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5322.C1","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"5 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130798817","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Correction: Reactivation of VKF Wind Tunnel D by AFRL at AEDC: Overview and Subsystem Checkout Results 修正:在AEDC由AFRL重新激活VKF风洞D:概述和子系统检验结果
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5263.C1
Jerrod W. Hofferth, Daniel R. Ogg
{"title":"Correction: Reactivation of VKF Wind Tunnel D by AFRL at AEDC: Overview and Subsystem Checkout Results","authors":"Jerrod W. Hofferth, Daniel R. Ogg","doi":"10.2514/6.2018-5263.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5263.C1","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125300997","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Correction: Preliminary Qualitative Observations of Ignition Phenomena in Rotating Detonation Engines 修正:旋转爆震发动机点火现象的初步定性观察
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5199.C1
A. Mizener, C. J. Green, F. Lu
{"title":"Correction: Preliminary Qualitative Observations of Ignition Phenomena in Rotating Detonation Engines","authors":"A. Mizener, C. J. Green, F. Lu","doi":"10.2514/6.2018-5199.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5199.C1","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"22 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132046685","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Correction: Effects of Variable Wall Temperature Distributions on 3D Boundary Layers 修正:变壁面温度分布对三维边界层的影响
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5271.C1
J. Thome, John D. Reinert, A. Dwivedi, G. Candler
{"title":"Correction: Effects of Variable Wall Temperature Distributions on 3D Boundary Layers","authors":"J. Thome, John D. Reinert, A. Dwivedi, G. Candler","doi":"10.2514/6.2018-5271.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5271.C1","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"38 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116133891","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Correction: SpaceLiner Cabin Escape System Design and Simulation of Emergency Separation from its Winged Stage 修正:航天飞机客舱逃生系统设计及与翼级紧急分离仿真
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5255.C1
S. Stappert, M. Sippel, Leonid Bussler, Jascha Wilken, Sven Krummen
{"title":"Correction: SpaceLiner Cabin Escape System Design and Simulation of Emergency Separation from its Winged Stage","authors":"S. Stappert, M. Sippel, Leonid Bussler, Jascha Wilken, Sven Krummen","doi":"10.2514/6.2018-5255.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5255.C1","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130629954","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Preliminary Studies on Hypersonic Flows Over 3D Printed Models 3D打印模型上高超声速流动的初步研究
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-15 DOI: 10.2514/6.2018-5321
I. Rêgo, T. V. Marcos, V. Galvão, R. G. Vilela, M. Minucci, J. F. A. Martos, A. C. Oliveira
{"title":"Preliminary Studies on Hypersonic Flows Over 3D Printed Models","authors":"I. Rêgo, T. V. Marcos, V. Galvão, R. G. Vilela, M. Minucci, J. F. A. Martos, A. C. Oliveira","doi":"10.2514/6.2018-5321","DOIUrl":"https://doi.org/10.2514/6.2018-5321","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"13 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122376083","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Analysis of the Two-Level NO PLIF Model for Low-Temperature High-Speed Flow Applications 低温高速流动的两级NO PLIF模型分析
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-15 DOI: 10.2514/6.2018-5379
T. Drozda, Cody R. Ground, A. Ziltz, K. Cabell, J. Inman, B. Bathel, P. Danehy
{"title":"Analysis of the Two-Level NO PLIF Model for Low-Temperature High-Speed Flow Applications","authors":"T. Drozda, Cody R. Ground, A. Ziltz, K. Cabell, J. Inman, B. Bathel, P. Danehy","doi":"10.2514/6.2018-5379","DOIUrl":"https://doi.org/10.2514/6.2018-5379","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"245 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122467099","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 3
Development of a Rapid Inviscid/Boundary-Layer Aerodynamics Tool 一种快速无粘/边界层空气动力学工具的研制
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-15 DOI: 10.2514/6.2018-5270
Alexander Ward, M. Smart, R. Gollan
{"title":"Development of a Rapid Inviscid/Boundary-Layer Aerodynamics Tool","authors":"Alexander Ward, M. Smart, R. Gollan","doi":"10.2514/6.2018-5270","DOIUrl":"https://doi.org/10.2514/6.2018-5270","url":null,"abstract":"Hypersonic vehicles, combined with scramjet propulsion, offer significant and unique flexibility, performance and reusability benefits over rockets. These characteristics will likely reduce the cost of access-to-space. However, the realisation of such vehicles is significantly complicated by engine performance requirements which dictate relatively low altitude, high dynamic pressure trajectories. The thick atmosphere and high velocities result in high aerodynamic drag and heating. This paper introduces a simple, aerothermodynamic model for the analysis of hypersonic vehicles using Cart3D to calculate the inviscid flow-field and provide edge conditions to boundary layer calculations. Comparisons are made between two viscous methods of varying fidelity; flat plate correlations for skin friction with a simplified running length calculation and integral methods applied along inviscid, surface streamlines. Three validation cases are presented; (1) a hypersonic, blunt body; (2) a delta-wing, lifting body at subsonic to hypersonic Mach numbers and (3) a hypersonic, realistic vehicle configuration with internal flow-paths. In general, Cart3D predicts the lift and pitching moment coefficients well but consistently under-predicts drag given the absence of shear stress. The viscous contribution to aerodynamic forces was found to be adequately modelled using flat plate correlations and a simple Euclidean distance in place of the true running length. Preliminary results, however, suggest predictions of surface heat transfer rates benefit from a streamline running length and higher fidelity boundary layer methods.","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"26 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114599259","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 4
Heat Transfer Studies on Blunt Nosed Configurations in Hypersonic flow Subject to Normal and Tangential blowing 高超声速流中正吹和切向吹钝鼻结构的换热研究
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-15 DOI: 10.2514/6.2018-5168
M. Khalid, K. Juhany
{"title":"Heat Transfer Studies on Blunt Nosed Configurations in Hypersonic flow Subject to Normal and Tangential blowing","authors":"M. Khalid, K. Juhany","doi":"10.2514/6.2018-5168","DOIUrl":"https://doi.org/10.2514/6.2018-5168","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"55 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124517716","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Influence of hypersonic fluid-structure interaction on the control authority of a trailing-edge flap 高超声速流固耦合对尾缘襟翼控制权威的影响
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference Pub Date : 2018-09-15 DOI: 10.2514/6.2018-5265
S. Bhattrai, L. McQuellin, G. Currao, A. Neely, D. Buttsworth
{"title":"Influence of hypersonic fluid-structure interaction on the control authority of a trailing-edge flap","authors":"S. Bhattrai, L. McQuellin, G. Currao, A. Neely, D. Buttsworth","doi":"10.2514/6.2018-5265","DOIUrl":"https://doi.org/10.2514/6.2018-5265","url":null,"abstract":"","PeriodicalId":258669,"journal":{"name":"22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115845320","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 6
下一页 尾页
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整，为了账户安全，请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
请完成安全验证×
相关产品
×
本文献相关产品
联系我们：info@booksci.cn Book学术提供免费学术资源搜索服务，方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号：604180095
Book学术官方微信
小红书