Welcome to IJSDR UGC CARE norms ugc approved journal norms IJRTI Research Journal | ISSN : 2455-2631
International Peer Reviewed & Refereed Journals, Open Access Journal
ISSN Approved Journal No: 2455-2631 | Impact factor: 8.15 | ESTD Year: 2016
Scholarly open access journals, Peer-reviewed, and Refereed Journals, Impact factor 8.15 (Calculate by google scholar and Semantic Scholar | AI-Powered Research Tool) , Multidisciplinary, Monthly, Indexing in all major database & Metadata, Citation Generator, Digital Object Identifier(DOI)

Issue: August 2022

Volume 7 | Issue 8

Impact factor: 8.15

Click Here For more Info

Imp Links for Author
Imp Links for Reviewer
Research Area
Subscribe IJSDR
Visitor Counter

Copyright Infringement Claims
Indexing Partner
Published Paper Details
Authors Name: Amandeep Singh
Unique Id: IJSDR2010034
Published In: Volume 5 Issue 10, October-2020
Abstract: In this proposed paper the aerodynamic characteristics of an anti-aircraft missile were computed using Computational fluid dynamics by ANYS2020R1 software which is analysis software. Generally predicting the aerodynamic characteristics is mandatory in case of performance analysis. Aerodynamic characteristics are important role in missile aerodynamic because on the basis of results we conclude that missile design is stable or not and how they behave when missile is in cruise stage. Aerodynamic coefficient are Drag ,Drag coefficient, moment, moment coefficient characterization is carried out at subsonic & supersonic speed with their Mach number’s at standard sea level. The motivation of such work is caused due to lack of data on missile aerodynamic at supersonic level .The object moving at high speed induced the drag which decrease the velocity and affect the efficiencies of object. Now days we are moving towards high speed vehicle. By high speed vehicle, we save our time and more accurate on target like in defence system we use the different ballistic missile for targeting the object. Designing field give the ability to make more efficient body design for Aerospace Industry. By this paper we develop prototype missile design with accurate aerodynamics.
Keywords: Missile, Drag, Drag Coefficient, moment, moment coefficient, AOA (Angle of Attack)
Cite Article: "AERODYNAMIC ANALYSIS ON MISSILE DESIGN ", International Journal of Science & Engineering Development Research (www.ijsdr.org), ISSN:2455-2631, Vol.5, Issue 10, page no.255 - 262, October-2020, Available :http://www.ijsdr.org/papers/IJSDR2010034.pdf
Downloads: 000101774
Publication Details: Published Paper ID: IJSDR2010034
Registration ID:192638
Published In: Volume 5 Issue 10, October-2020
DOI (Digital Object Identifier):
Page No: 255 - 262
Publisher: IJSDR | www.ijsdr.org
ISSN Number: 2455-2631

Click Here to Download This Article

Article Preview

Click here for Article Preview

Major Indexing from www.ijsdr.org
Google Scholar ResearcherID Thomson Reuters Mendeley : reference manager Academia.edu
arXiv.org : cornell university library Research Gate CiteSeerX DOAJ : Directory of Open Access Journals
DRJI Index Copernicus International Scribd DocStoc

Track Paper
Important Links
Conference Proposal
DOI (A digital object identifier)

Providing A digital object identifier by DOI
How to GET DOI and Hard Copy Related
Open Access License Policy
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Creative Commons License
This material is Open Knowledge
This material is Open Data
This material is Open Content
Social Media

Indexing Partner