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
Selection of nozzle contours for a research scramjet engine.Scramjet engine nozzle contours noting expansion- deflection, bell, plug and arbitrary annular nozzles, with optimum nozzle design and computer program for performance prediction
Document ID
19670055198
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gaede, A. E.
Lopez, H. J.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 67-453
Report Number: AIAA PAPER 67-453
Accession Number
67A33927
Funding Number(s)
CONTRACT_GRANT: NAS1-5116
Distribution Limits
Public
Copyright
Other
Keywords
NOZZLE GEOMETRY
COMPUTER PROGRAM
PERFORMANCE PREDICTION
SCRAMJET ENGINE

Available Downloads

There are no available downloads for this record.

Related Records

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