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The Effects of Blowing Over Various Trailing-edge Flaps on an NACA 0006 Airfoil Section, Comparisons with Various Types of Flaps on other Airfoil Sections, and an Analysis of Flow and Power Relationships for Blowing SystemsThe results are presented of a two-dimensional investigation conducted to determine the effect of blowing over various types of trailing-edge flaps on a wing having the NACA 0006 airfoil section and a drooped-nose flap. The position and profile of the trailing-edge flap, the nozzle height, and the location of the flap with respect to the nozzle were found to be important variables. Data from many investigations were used to make an evaluation of the effects of blowing on lift. An analysis was made of flow and power relationships for blowing systems.
Document ID
19760025045
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Dods, J. B., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Watson, E. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
A-6423
NASA-TN-D-8293
Report Number: A-6423
Report Number: NASA-TN-D-8293
Accession Number
76N32133
Funding Number(s)
PROJECT: RTOP 506-17-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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