NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
A mixing augmentation technique for hypervelocity scramjetsThe paper discusses mixing problems in hypervelocity scramjet combustors. Techniques for providing turbulence and/or mixing enhancement are described. One such technique, the oscillating shock interaction, is studied numerically and options for producing oscillatory shock waves for mixing augmentation in scramjet combustors are discussed.
Document ID
19870058001
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kumar, A. (NASA Langley Research Center Hampton, VA, United States)
Bushnell, D. M. (NASA Langley Research Center Hampton, VA, United States)
Hussaini, M. Y. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 87-1882
Report Number: AIAA PAPER 87-1882
Accession Number
87A45275
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available