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
High-speed Stability and Control Characteristics of a Fighter Airplane Model with a Swept-back Wing and Tail
Document ID
19930085821
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morrill, Charles P , Jr
Boddy, Lee E
Date Acquired
August 16, 2013
Publication Date
April 14, 1948
Report/Patent Number
NACA-RM-A7K28
Report Number: NACA-RM-A7K28
Accession Number
93R15111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available