NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Exploratory Investigation of the Effect of Wing Slots and Leading-edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-fuselage Configuration
Document ID
19930089692
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Critzos, Chris C
Date Acquired
August 16, 2013
Publication Date
February 8, 1957
Report/Patent Number
NACA-RM-L56L06
Report Number: NACA-RM-L56L06
Accession Number
93R18982
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