Actions for Application of CFD codes for the simulation of scramjet combustor flowfields

Email RIS file
Bookmark
Report an Issue

Application of CFD codes for the simulation of scramjet combustor flowfields

Author
Northam, G. Burton
Published
Sep 1, 1989.
Physical Description
1 electronic document
Additional Creators
Chitsomboom, Tawit
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
An overview of CFD activities in the Hypersonic Propulsion Branch is given. Elliptic and PNS codes that are being used for the simulation of hydrogen-air combusting flowfields for scramjet applications are discussed. Results of the computer codes are shown in comparison with those of the experiments where applicable. Two classes of experiments will be presented: parallel injection of hydrogen into vitiated supersonic air flow; and normal injection of hydrogen into supersonic crossflow of vitiated air.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19910001560.
Accession ID: 91N10873.
NASA, Ames Research Center, NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12; p 75-89.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15684126