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Procedures for the design of low-pitching-moment airfoilsThe pitching moment of a given airfoil is decreased by specifying appropriate modifications to its pressure distribution; by prescribing parameters in a special formula for the Theodorsen epsilon-function; and with superposition of a thickness distribution and subsequent tailoring. Advantages and disadvantages of the three methods are discussed.
Document ID
19750019932
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Barger, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Aeronautics (General)
Report/Patent Number
L-10114
NASA-TN-D-7982
Report Number: L-10114
Report Number: NASA-TN-D-7982
Accession Number
75N28004
Funding Number(s)
PROJECT: RTOP 505-06-31-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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