NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Two-dimensional Wind-tunnel Investigation of the NACA 64(sub 1)-012 Airfoil Equipped with Two Types of Leading-edge Flap
Document ID
19930081893
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fullmer, Felicien F
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1277
Report Number: NACA-TN-1277
Accession Number
93R11183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 641-012 - CHAR ,MOMENTS & ORDINATES
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2 X 3')
WORK CARRIED ON AT LAL
AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS
WINGS - HIGH LIFT DEVICES
LOW-DRAG (WING FLAPS)
WING FLAPS, SPLIT
WING FLAPS, LEADING-EDGE

Related Records

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