NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Design of optimized three-dimensional nozzles.Optimization of supersonic portion of three- dimensional flow geometry in rocket motor nozzle for maximum thrust
Document ID
19660061818
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Murthy, S. N. B.
Thompson, H. D.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-568
Report Number: AIAA PAPER 65-568
Accession Number
66A41108
Distribution Limits
Public
Copyright
Other
Keywords
THREE-DIMENSIONAL FLOW
OPTIMUM THRUST PROGRAMMING
SUPERSONIC NOZZLE
ROCKET NOZZLE
NOZZLE FLOW

Available Downloads

There are no available downloads for this record.

Related Records

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