NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds
Document ID
19930087384
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gillis, Clarence L
Chapman, Rowe, Jr
Date Acquired
August 16, 2013
Publication Date
January 22, 1953
Report/Patent Number
NACA-RM-L52K20
Report Number: NACA-RM-L52K20
Accession Number
93R16674
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available