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Tests in the Variable-Density Wind Tunnel of Related Airfoils Having the Maximum Camber Unusually Far ForwardA family of related airfoils having the position of maximum camber unusually far forward was investigated in the variable-density tunnel as an extension of the study recently completed of a large number of related airfoils. The new airfoils gave improved characteristics over those previously investigated, especially in regard to the pitching moment. Some of the new sections are markedly superior to well-known and commonly used sections and should replace them in applications requiring a slightly cambered section of moderate thickness having a small pitching-moment coefficient.
Document ID
19930091610
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Report
Authors
Eastman N Jacobs
(Langley Memorial Aeronautical Laboratory Hampton, United States)
Robert M Pinkerton
(Langley Memorial Aeronautical Laboratory Hampton, United States)
Date Acquired
September 6, 2013
Publication Date
May 7, 1935
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aerodynamics
Report/Patent Number
NACA-TR-537
Accession Number
93R20900
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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