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
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodiesEffect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersonic engine nacelles
Document ID
19680009768
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Shrewsbury, G. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1517
Report Number: NASA-TM-X-1517
Accession Number
68N19237
Funding Number(s)
CONTRACT_GRANT: 720-03-01-08-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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