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
Low-speed Measurement of Tail Contribution to Rolling Stability Derivatives and Air-flow Angularity at the Tail for an X-tail Model in Steady Roll Including Some Effects of Wing-tip Stores
Document ID
19930089436
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Riley, Donald R
Date Acquired
August 16, 2013
Publication Date
November 23, 1956
Report/Patent Number
NACA-RM-L56I21
Report Number: NACA-RM-L56I21
Accession Number
93R18726
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