NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
NASA supercritical airfoils: A matrix of family-related airfoilsThe NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented.
Document ID
19900007394
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Harris, Charles D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-2969
L-16625
NAS 1.60:2969
Accession Number
90N16710
Funding Number(s)
PROJECT: RTOP 505-61-21-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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