NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Stability and Control Characteristics at Low Speed of an Airplane Model Having a 38.7 Degree Sweptback Wing with Aspect Ratio 4.51, Taper Ratio 0.54, and Conventional Tail Surfaces
Document ID
19930082364
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lockwood, Vernard E
Watson, James M
Date Acquired
August 16, 2013
Publication Date
December 1, 1948
Report/Patent Number
NACA-TN-1742
Report Number: NACA-TN-1742
Accession Number
93R11654
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FINS, VENTRAL
STALLING
AIRFOILS, CIRCULAR-ARC
WING SLOTS
WINGS - DIHEDRAL
TAIL SURFACES
STABILITY & CONTROL
WING FLAPS, LEADING-EDGE
INTERFERENCE - WINGS & FUSELAGES
WINGS, SWEPTBACK

Related Records

There are no records associated with this record.
No Preview Available