المؤلفون: S. J. Hu, Z. J. Wei, M. Ni, G. M. Ren

المصدر: Journal of Applied Fluid Mechanics, Vol 17, Iss 12, Pp 2791-2806 (2024)

مصطلحات موضوعية: leading, edge sawtooth transonic compressor cascade cascade characteristics aerodynamic shock wave /boundary layer interaction, Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: https://www.jafmonline.net/article_2530_aeb180124409d687089682d7aefc7abc.pdf; https://doaj.org/toc/1735-3572; https://doaj.org/toc/1735-3645

URL الوصول: https://doaj.org/article/6ef5c87fa72a4f998ca3dc8ed8c5c4cd

المؤلفون: Vishal Umapathi Choudhari, Keerthi J S, Gopalakrishna N

المصدر: Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 2, Pp 107-121 (2024)

مصطلحات موضوعية: shock wave, shock wave/boundary layer interaction, diameter of cylinder, boundary layer, separation bubble and surface pressure, Technology, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://jast.hho.msu.edu.tr/index.php/JAST/article/view/594/420; https://doaj.org/toc/1304-0448; https://doaj.org/toc/2148-1059

URL الوصول: https://doaj.org/article/abada65341754532b4b6e061138a0700

المؤلفون: Kunhang Li, Bo Song, Suyu Jiang, Jiao Wang, Xiaojun Fan, Jingyin Li

المصدر: Aerospace, Vol 12, Iss 1, p 25 (2024)

مصطلحات موضوعية: F-class heavy-duty gas turbine, transonic compressor, shock wave/boundary layer interaction, flow analysis, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2226-4310/12/1/25; https://doaj.org/toc/2226-4310

URL الوصول: https://doaj.org/article/951564033f5e4b7984215292aeb33892

المؤلفون: Jian Qin, Haichuan Yu, Jie Wu

المصدر: Advances in Aerodynamics, Vol 6, Iss 1, Pp 1-21 (2024)

مصطلحات موضوعية: Shock wave/boundary layer interaction, High order method, Flux reconstruction, Lattice Boltzmann flux solver, Entropy-based adaptive filtering method, Engineering (General). Civil engineering (General), TA1-2040, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://doaj.org/toc/2524-6992

URL الوصول: https://doaj.org/article/d3d58470044c4f11aa3ceed9654c13c2

المؤلفون: Bei Wang, Cosimo Corsi, Thomas Weiland, Zhenyu Wang, Thomas Grund, Olaf Pohl, Johannes Max Bienia, Julien Weiss, Ha Duong Ngo

المصدر: Micromachines, Vol 15, Iss 12, p 1423 (2024)

مصطلحات موضوعية: supersonic, shock wave/boundary layer interaction (SWBLI), PVDF, piezoelectric pressure transduce, FEM simulation, dynamic response in frequency domain, Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2072-666X/15/12/1423; https://doaj.org/toc/2072-666X

URL الوصول: https://doaj.org/article/29a90c82fb8b4b20990a803dea955961

المؤلفون: Threadgill, James, Hader, Christoph, Singh, Ashish, Tsakagiannis, Vasilis, Fasel, Hermann, Little, Jesse, Lugrin, Mathieu, Bur, Reynald, Chiapparino, Giuseppe, Stemmer, Christian

المساهمون: Department of Aerospace and Mechanical Engineering Tucson, University of Arizona, The Ohio State University Columbus (OSU), DAAA, ONERA, Institut Polytechnique de Paris Meudon, ONERA-Institut Polytechnique de Paris (IP Paris), Technische Universität Munchen - Technical University Munich - Université Technique de Munich (TUM), CEA 4600334751

المصدر: AIAA SCITECH 2024 Forum ; https://hal.science/hal-04453027 ; AIAA SCITECH 2024 Forum, Jan 2024, Orlando, United States. ⟨10.2514/6.2024-0498⟩

مصطلحات موضوعية: shock-wave boundary layer interaction, free-stream noise, hypersonic, sbli, ioccl, interaction onde de choc couche limite, perturbation d'écoulement libre, hypersonique, [PHYS]Physics [physics], [SPI]Engineering Sciences [physics]

جغرافية الموضوع: Orlando, United States

Relation: hal-04453027; https://hal.science/hal-04453027; https://hal.science/hal-04453027/document; https://hal.science/hal-04453027/file/scaling_and_transitionEffects_on_hollowCylinder.pdf

الاتاحة: https://hal.science/hal-04453027
https://hal.science/hal-04453027/document
https://hal.science/hal-04453027/file/scaling_and_transitionEffects_on_hollowCylinder.pdf
https://doi.org/10.2514/6.2024-0498

المؤلفون: Y. Li, Z. Wu, S. Wu, S. Hu, F. Wei

المصدر: Journal of Applied Fluid Mechanics, Vol 16, Iss 9, Pp 1865-1876 (2023)

مصطلحات موضوعية: hypersonic inlet, busemann inlet, large eddy simulation, total pressure distortion, swirl distortion, shock wave–boundary layer interaction, Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: https://www.jafmonline.net/article_2267_1d75813febba2b0e63c137241b3a6365.pdf; https://doaj.org/toc/1735-3572; https://doaj.org/toc/1735-3645

URL الوصول: https://doaj.org/article/b4ee78fc2710442f8586892f5a4b33a5

المؤلفون: Hongyu Wang, Xiaohua Fan, Yanguang Yang, Gang Wang, Feng Xie

المصدر: Fluids, Vol 9, Iss 8, p 173 (2024)

مصطلحات موضوعية: shock wave/boundary layer interaction, experimental fluid mechanics, convolutional neural networks, high speed flows, wall pressure prediction, Thermodynamics, QC310.15-319, Descriptive and experimental mechanics, QC120-168.85

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2311-5521/9/8/173; https://doaj.org/toc/2311-5521

URL الوصول: https://doaj.org/article/713fe072a8a549c58a3f48051ab82d95

المؤلفون: Soldati, Giulio, Ceci, Alessandro, Pirozzoli, Sergio

المساهمون: Soldati, Giulio, Ceci, Alessandro, Pirozzoli, Sergio

مصطلحات موضوعية: high speed compressible flow, energy preserving generalised curvilinear coordinate, computational fluid dynamic, shock wave/boundary layer interaction

Relation: numberofpages:13; journal:AEROTECNICA MISSILI E SPAZIO; https://hdl.handle.net/11573/1703805

الاتاحة: https://hdl.handle.net/11573/1703805
https://doi.org/10.1007/s42496-024-00199-4

المؤلفون: Yue, L, Jia, Y, Xu, X, Zhang, X, Zhang, P

المساهمون: Department of Mechanical Engineering

مصطلحات موضوعية: Cowl shock, Inlet restart, Shock wave boundary layer interactions

Relation: http://hdl.handle.net/10397/106499; 72; 80; 74; 2-s2.0-85041480852; ME-0681

الاتاحة: http://hdl.handle.net/10397/106499
https://doi.org/10.1016/j.ast.2017.12.018

المؤلفون: Fangyou Yu, Zhanbiao Gao, Qifan Zhang, Lianjie Yue, Hao Chen

المصدر: Aerospace, Vol 11, Iss 2, p 148 (2024)

مصطلحات موضوعية: micro-serration, separation control, shock wave/boundary layer interaction, Motor vehicles. Aeronautics. Astronautics, TL1-4050

Relation: https://www.mdpi.com/2226-4310/11/2/148; https://doaj.org/toc/2226-4310; https://doaj.org/article/69f6473a09994670a4005d7ca5eeae8a

الاتاحة: https://doi.org/10.3390/aerospace11020148
https://doaj.org/article/69f6473a09994670a4005d7ca5eeae8a

المؤلفون: Linyang Zhu, Tian Wang, Qilong Guo, Xianxu Yuan

المصدر: Engineering Applications of Computational Fluid Mechanics, Vol 17, Iss 1 (2023)

مصطلحات موضوعية: Shock wave/boundary layer interaction, k-ω SST turbulence model, Neural network, Stress limiter, Engineering (General). Civil engineering (General), TA1-2040

وصف الملف: electronic resource

Relation: https://doaj.org/toc/1994-2060; https://doaj.org/toc/1997-003X

URL الوصول: https://doaj.org/article/6058d66123fa45a9a1c5439cfe85518c

المؤلفون: Liu-qing YANG, Qin LI, Yan-cheng YOU

المصدر: 气体物理, Vol 8, Iss 1, Pp 36-47 (2023)

مصطلحات موضوعية: oblique shock wave, shock wave/boundary-layer interactions, three-dimensional effects, numerical simulation, parametric study, Astrophysics, QB460-466

وصف الملف: electronic resource

Relation: https://doaj.org/toc/2096-1642

URL الوصول: https://doaj.org/article/639b5fb2c5994bf3a028aec02f6df6d1

المؤلفون: Xu Hao, Du Zhaobo, Zhong Xiangyu, Huang Wei

المصدر: Hangkong bingqi, Vol 29, Iss 4, Pp 83-90 (2022)

مصطلحات موضوعية: shock wave/boundary layer interactions, flow separation, microjet, flow control, vortex pair, flow field, supersonic vehicle, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00054.pdf; https://doaj.org/toc/1673-5048

URL الوصول: https://doaj.org/article/652a53850eab445e8c69537f80dd8034

المؤلفون: Simin Gao, Hexia Huang, Yupeng Meng, Huijun Tan, Mengying Liu, Kun Guo

المصدر: Aerospace, Vol 10, Iss 12, p 1021 (2023)

مصطلحات موضوعية: wind shear, hypersonic inlet/isolator, shock wave/boundary layer interaction, shock train, unsteady simulation, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2226-4310/10/12/1021; https://doaj.org/toc/2226-4310

URL الوصول: https://doaj.org/article/c57ac070e085415abde46c4c1cfea814

المؤلفون: A. Nazarian Shahrbabaki, R. Khoshkhoo, M. Bazazzadeh

المصدر: Journal of Applied Fluid Mechanics, Vol 15, Iss 4, Pp 1035-1047 (2022)

مصطلحات موضوعية: span-wise/stream-wise actuation, nanosecond dbd, plasma actuator, flow separation, shock wave/boundary layer interaction, Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: https://www.jafmonline.net/article_2047_7c860e6d93db871dcb9ea0a706c42b35.pdf; https://doaj.org/toc/1735-3572; https://doaj.org/toc/1735-3645

URL الوصول: https://doaj.org/article/60b114be8155456d87044382226bf76c

المؤلفون: Mengge Wang, Ziyun Wang, Yue Zhang, Daishu Cheng, Huijun Tan, Kun Wang, Simin Gao

المصدر: Aerospace; Volume 10; Issue 8; Pages: 729

مصطلحات موضوعية: dynamic micro-vortex generator, shock wave/boundary layer interaction, dynamic grid simulation, flow control, supersonic inlet

وصف الملف: application/pdf

Relation: Aeronautics; https://dx.doi.org/10.3390/aerospace10080729

الاتاحة: https://doi.org/10.3390/aerospace10080729

المؤلفون: Davide Di Pasquale, Simon Prince

المصدر: Aerospace; Volume 10; Issue 6; Pages: 569

مصطلحات موضوعية: transonic aerodynamics, shock wave boundary layer interaction, passive flow control, surface roughness, buffet alleviation, experiment

وصف الملف: application/pdf

Relation: Aeronautics; https://dx.doi.org/10.3390/aerospace10060569

الاتاحة: https://doi.org/10.3390/aerospace10060569

المؤلفون: John-Paul Mosele, Andreas Gross, John Slater

المصدر: Aerospace; Volume 10; Issue 5; Pages: 417

مصطلحات موضوعية: supersonic flow, asymmetric flow, shock wave boundary layer interaction, turbulent separation, unsteady flow, large-eddy simulation, crossflow

وصف الملف: application/pdf

Relation: Aeronautics; https://dx.doi.org/10.3390/aerospace10050417

الاتاحة: https://doi.org/10.3390/aerospace10050417

المؤلفون: Zhongqi Luo, Hexia Huang, Huijun Tan, Gang Liang, Jinghao Lv, Yuwen Wu, Liugang Li

المصدر: Aerospace; Volume 10; Issue 2; Pages: 188

مصطلحات موضوعية: terminal shock wave/moving shock wave/boundary layer interaction, rotating denotation wave, helical vortex, isolator

وصف الملف: application/pdf

Relation: Aeronautics; https://dx.doi.org/10.3390/aerospace10020188

الاتاحة: https://doi.org/10.3390/aerospace10020188