NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Corrections for lift, drag, and moment of an airfoil in a supersonic tunnel having a given static pressure gradient
Document ID
19930083566
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ludloff, H F (New York University)
Friedman, M B (New York University)
Date Acquired
August 16, 2013
Publication Date
December 1, 1952
Report/Patent Number
NACA-TN-2849
Accession Number
93R12856
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