NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight-determined Static Lateral Stability and Control Characteristics of a Swept-wing Fighter Airplane to a Mach Number of 1.39
Document ID
19930089538
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Matranga, Gene J
Peele, James R
Date Acquired
August 16, 2013
Publication Date
March 11, 1957
Report/Patent Number
NACA-RM-H57A16
Report Number: NACA-RM-H57A16
Accession Number
93R18828
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available