Performance of some Limiters on the Higher Order Computation of Inviscid Hypersonic Flows
Clicks: 187
ID: 13854
2016
Article Quality & Performance Metrics
Overall Quality
Not rated
Combines reader engagement with the AI quality analysis. This
article has not been analysed, so there is no overall score —
reader engagement is measured and shown alongside.
Reader Engagement
Steady Performance
71.8
/100
187 views
154 readers
Trending
AI Quality Assessment
Not analyzed
Readership in this journal
SteadyRanked #115 of 148 articles by views in adbu journal of engineering technology
Most read
Least read
Bar heights use a square-root scale. Only the 120 most-read articles are drawn; the journal has 148 in total.
Mint this article as an NFT
Not yet mintedCreate a permanent, verifiable on-chain record of this article on the Scimatic Network. The NFT is held in your Journament account, and you can withdraw it to your own wallet at any time.
5
SUSD
one-off · no wallet required
Abstract
The Advection Upstream Splitting Method (AUSM) is used to compute 2D inviscid hypersonic flow over a semi-cylinder on a finite volume framework. Solution reconstruction to achieve higher order accuracy is done using the MUSCL-type reconstruction technique with the Van Albada and Hemker-Koren limiter functions. The gas models under consideration are the perfect gas model and the high temperature equilibrium chemically reacting air model of Tannehill and Mugge. The performance of these limiters in computing hypersonic flows is analyzed and compared with the first order accurate method. Keywords:Hypersonic, shock, reconstruction, limiter
Abstract Quality Issue:
This abstract appears to be incomplete or contains metadata (91 words).
Try re-searching for a better abstract.
| Reference Key |
kalita2016performanceadbu
Use this key to autocite in the manuscript while using
SciMatic Manuscript Manager or Thesis Manager
|
|---|---|
| Authors | Abhijit Gogoi, Paragmoni Kalita; |
| Journal | adbu journal of engineering technology |
| Year | 2016 |
| DOI |
DOI not found
|
| URL | |
| Keywords | Keywords not found |
Citations
No citations found. To add a citation, contact the admin at info@scimatic.org
Comments
No comments yet. Be the first to comment on this article.