NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Effect of Spoiler-type Lateral-control Devices on the Twisting Moments of NACA 230-series Airfoil Sections
Document ID
19930081922
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fitzpatrick, James E
Furlong, G Chester
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1298
Report Number: NACA-TN-1298
Accession Number
93R11212
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, TWISTED
LATERAL CONTROL DEVICES WORK CARRIED ON AT AAL
PRESSURE DISTRIBUTION - AIRFOILS - NACA 230-SERIES
WING - BENDING & TORSION
LOAD DISTRIBUTION, WING-SPAN
AIRFOILS - NACA 23009
AIRFOILS - NACA 230-SERIES - CHAR & MOMENTS WING SPOILERS
WING SPOILERS
AIRFOILS - NACA 23016
WIND TUNNEL TESTS - NACA - PRESSURE (19') WORK CARRIED ON AT LMAL

Related Records

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