NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions
Document ID
19930088723
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spreemann, Kenneth P
Date Acquired
August 29, 2013
Publication Date
July 21, 1955
Report/Patent Number
NACA-RM-L55E25a
Report Number: NACA-RM-L55E25a
Accession Number
93R18013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available