NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wind-tunnel Investigation of the Effects of Lip Geometry on Drag and Pressure Recovery of a Normal-shock Nose Inlet on a Body of Revolution at Mach Numbers of 1.41 and 1.81
Document ID
19930090403
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Robins, A Warner
Date Acquired
August 15, 2013
Publication Date
February 3, 1958
Report/Patent Number
NACA-RM-L57K08
Accession Number
93R19693
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