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
High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane-dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1
Document ID
19930085531
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Robinson, Harold L
Date Acquired
August 16, 2013
Publication Date
November 4, 1948
Report/Patent Number
NACA-RM-L8H05
Report Number: NACA-RM-L8H05
Accession Number
93R14821
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