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
Boundary-layer combustion in propulsion.Propulsion-oriented subsonic boundary layer combustion research, discussing turbulent and diffusion-limited conditions, radiant heat transfer, chemical kinetics and transient phenomena
Document ID
19670055071
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marxman, G. A.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Thermodynamics And Combustion
Accession Number
67A33800
Funding Number(s)
CONTRACT_GRANT: NGR-39-003-005
CONTRACT_GRANT: DA-ARO/D/-31-124-G841
CONTRACT_GRANT: NAS7-389
CONTRACT_GRANT: NSF GP-5734
CONTRACT_GRANT: AF-AFOSR/638/-1367
Distribution Limits
Public
Copyright
Other
Keywords
RADIATIVE HEAT TRANSFER
BOUNDARY LAYER COMBUSTION
CHEMICAL KINETICS
PROPULSION SYSTEM

Available Downloads

There are no available downloads for this record.

Related Records

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