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
Comparison of wind tunnel and flight-measured base pressures from the sharp-leading-edge upper vertical fin of the X-15 airplane for turbulent flow at Mach numbers from 1.5 to 5.0Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared with wind tunnel data for turbulent flow at Mach numbers from 1.5 to 5.0
Document ID
19710014446
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Goecke, S. A. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-6348
H-602
Report Number: NASA-TN-D-6348
Report Number: H-602
Accession Number
71N23922
Funding Number(s)
CONTRACT_GRANT: 722-51-00-01-24
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