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
High-speed Tests of an Airfoil Section Cambered to Have Critical Mach Numbers Higher than Those Attainable with a Uniform-load Mean Line
Document ID
19930082040
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Graham, Donald J
Date Acquired
August 16, 2013
Publication Date
July 1, 1947
Report/Patent Number
NACA-TN-1396
Report Number: NACA-TN-1396
Accession Number
93R11330
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY
WORK CARRIED ON AT AAL
PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(109)-210
ORDINATES - LOW-DRAG
AIRFOILS - NACA 66-210 - CHAR & MOMENTS - LOW-DRAG
AIRFOILS - NACA 66(109)-210 (A=1 0,CLI=0 6)- CHAR ,MOMENTS & (A=0 6,CLI=-0 4)
WIND TUNNEL TESTS - AAL - HIGH-SPEED (3 1/2'X1')
AIRFOILS, CAMBERED - CHARACTERISTICS - WIND TUNNEL TESTS

Related Records

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