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
Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90Flight test evaluation of splitter plate in base drag reduction at subsonic speeds
Document ID
19670017229
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hintz, J. (NASA Flight Research Center Edwards, CA, United States)
Saltzman, E. J. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1376
Report Number: NASA-TM-X-1376
Accession Number
67N26558
Funding Number(s)
CONTRACT_GRANT: 126-16-05-02-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUBSONIC SPEED
DRAG REDUCTION
PLATE
FLIGHT TEST

Related Records

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