NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The development of satisfactory flying qualities on the Douglas dive bomber, model SBD-1 through flight testing successive modifications in control-surface area, hinge-line location, and aerodynamic-balance nose shape
Document ID
19930092599
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Root, L E
Date Acquired
September 6, 2013
Publication Date
May 1, 1942
Report/Patent Number
NACA-WR-W-81
Accession Number
93R21889
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STALLING - DOUGLAS SBD-1
STABILITY & CONTROL - DOUGLAS SBD-1
DIVING - PULL-OUTS - DOUGLAS SBD-1
AILERONS - BRISTOL FRISE
CONTROL STICKS - FORCES
AIRFOILS - TAIL SURFACE SECTIONS
WINGS - DIHEDRAL
TABS
CONTROL SURFACES, BALANCED - AERODYNAMIC
CONTROL SURFACES - DOUGLAS SBD-1
No Preview Available