UGC Approved Journal no 63975(19)

ISSN: 2349-5162 | ESTD Year : 2014
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Published in:

Volume 8 Issue 9
September-2021
eISSN: 2349-5162

UGC and ISSN approved 7.95 impact factor UGC Approved Journal no 63975

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Published Paper ID:
JETIR2109376


Registration ID:
315329

Page Number

d687-d693

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Title

A Review on Effect of Shock Wave Boundary Layer Interaction in different Flows Fields

Abstract

From past 50 years of research shock wave boundary interaction (SBLI) has played the most crucial role while designing the Air vehicle (like Rocket, Airplane, Missile, etc.,). Here considering ten different papers and deeply understanding the concept and reviewing the literature. The shock wave boundary layer interaction has various kinds of usages in the aerospace industry (like transonic and supersonic flight vehicle surfaces, and surfaces of rockets, missiles, transonic turbine blade passages, and re-entry vehicles, transonic gas turbine blade tip gaps, scramjet isolator ducts, supersonic aircraft engine intakes). Considering various applications mentioned above and taking the research paper for each application and reviewed which has been done in the paper through which medium. Considering the numerical method to determine the concept of shock boundary layer interaction (SBLI) and comparing the result with CFD to provide the data that attain in an efficient manner. And Conducting experiments through different wind tunnels (like LENS XX, transonic and supersonic wind tunnel) and comparing the result with CFD. Determining the dimension flow while conducting the experiment. Shock wave boundary layer interaction (SBLI) review based on different concepts of interacting profiles in different boundary-layer conditions on different models and applications.

Key Words

Shock wave, Boundary layer, SBLI, Transonic flow, Supersonic flow, Hypersonic flow, CFD, 2D flow and 3D flow.

Cite This Article

"A Review on Effect of Shock Wave Boundary Layer Interaction in different Flows Fields", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 9, page no.d687-d693, September-2021, Available :http://www.jetir.org/papers/JETIR2109376.pdf

ISSN


2349-5162 | Impact Factor 7.95 Calculate by Google Scholar

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 7.95 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Cite This Article

"A Review on Effect of Shock Wave Boundary Layer Interaction in different Flows Fields", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 9, page no. ppd687-d693, September-2021, Available at : http://www.jetir.org/papers/JETIR2109376.pdf

Publication Details

Published Paper ID: JETIR2109376
Registration ID: 315329
Published In: Volume 8 | Issue 9 | Year September-2021
DOI (Digital Object Identifier):
Page No: d687-d693
Country: KANCHIPURAM, TAMIL NADU, India .
Area: Science & Technology
ISSN Number: 2349-5162
Publisher: IJ Publication


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