NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
The effects of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with 45 degree sweptback wing
Document ID
19930082991
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hewes, Donald E
Date Acquired
August 29, 2013
Publication Date
March 1, 1951
Report/Patent Number
NACA-TN-2313
Report Number: NACA-TN-2313
Accession Number
93R12281
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY & CONTROL, LATERAL
STABILITY & CONTROL, DIRECTIONAL
STABILITY, LATERAL - DYNAMIC
AIRPLANES - MODELS - MASS DISTRIBUTION
STABILITY, DIRECTIONAL - DYNAMIC
No Preview Available