Numerical computations of steady transonic and supersonic flow fields (Record no. 814803)
[ view plain ]
000 -LEADER | |
---|---|
fixed length control field | 01748aab a2200217 4500 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 240125b19901990|||mr||| |||| 00| 0 eng d |
022 ## - INTERNATIONAL STANDARD SERIAL NUMBER | |
International Standard Serial Number | 0017-9310 |
100 ## - MAIN ENTRY--PERSONAL NAME | |
Personal name | A. Palacio. |
9 (RLIN) | 880248 |
100 ## - MAIN ENTRY--PERSONAL NAME | |
Personal name | M.R. Malin. |
9 (RLIN) | 880249 |
100 ## - MAIN ENTRY--PERSONAL NAME | |
Personal name | N. Proumen. |
9 (RLIN) | 880250 |
100 ## - MAIN ENTRY--PERSONAL NAME | |
Personal name | L. Sanchez. |
9 (RLIN) | 880251 |
245 ## - TITLE STATEMENT | |
Title | Numerical computations of steady transonic and supersonic flow fields |
300 ## - PHYSICAL DESCRIPTION | |
Extent | 1193-1204 p. |
520 ## - SUMMARY, ETC. | |
Summary, etc. | A prediction procedure for computing the shock and expansion waves associated with transonic and supersonic flow is presented. In order to assess the capability of the model, calculations are carried out for a number of benchmark cases, for which analytical solutions or published data are available. The cases considered are: supersonic flow over jet vanes; transonic shocked flow in a nozzle; over- and under-expanded free jets with Mach disc formation; and supersonic flow in a cascade of wedges with shock reflection and Prandtl-Meyer expansion. The model, which includes the solution of the steady-state Euler equations as well as the full Navier-Stokes equations, utilizes some modifications made to an existing finite-volume formulation in order to ensure momentum and energy conservation through the shock waves.<br/><br/>In all the cases, the calculations compare favourably with the analytical and experimental results.<br/> |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
Topical term or geographic name entry element | Numerical Computations |
9 (RLIN) | 815529 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
Topical term or geographic name entry element | Steady Transonic |
9 (RLIN) | 880252 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
Topical term or geographic name entry element | Supersonic Flow Fields |
9 (RLIN) | 880253 |
773 0# - HOST ITEM ENTRY | |
International Standard Serial Number | 00179310 |
Title | International Journal of Heat and Mass Transfer |
Place, publisher, and date of publication | New York, U.S.A : Pergamon Subsidiary of Elsevier Science & Technology |
856 ## - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | <a href="https://www.sciencedirect.com/science/article/pii/001793109090251O ">https://www.sciencedirect.com/science/article/pii/001793109090251O </a> |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Source of classification or shelving scheme | Dewey Decimal Classification |
Suppress in OPAC | No |
Koha item type | Articles |
-- | 14993 |
-- | Mr. Muhammad Rafique Al Haj Rajab Ali (Late) |
Not for loan | Home library | Serial Enumeration / chronology | Total Checkouts | Date last seen | Koha item type |
---|---|---|---|---|---|
Periodical Section | Vol.33, No.6 (June 1990) | 25/01/2024 | Articles |