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 : D-558-1 Speed-reduction Brake and Symmetrical-profile Wing Characteristics
Document ID
19930085315
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wright, John B
Date Acquired
August 16, 2013
Publication Date
June 15, 1948
Report/Patent Number
NACA-RM-L8B06
Report Number: NACA-RM-L8B06
Accession Number
93R14605
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