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An Evaluation of the Characteristics of a 10-percent-thick NACA 66-series Airfoil Section with a Special Mean-camber Line Designed to Produce a High Critical Mach Number
Document ID
19930082303
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Loftin, Laurence K
Cohen, Kenneth S
Date Acquired
August 16, 2013
Publication Date
July 1, 1948
Report/Patent Number
NACA-TN-1633
Report Number: NACA-TN-1633
Accession Number
93R11593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS
AIRFOILS - NACA 66(09)-210(1=1 0,C1I=0 6) - CHAR , MOMENTS & ORDINATES (A=0 6,C1
AIRFOILS - NACA 66-210 - CHAR & MOMENTS LOW-DRAG (WING FLAPS,SPLIT) PRESSURE D
AIRFOILS - NACA 66-210 (A=1 0,C1I=0 6) - CHAR , MOMENTS & ORDINATES (09) (A=0 6,

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