Experimental Results For The Eppler 387 Airfoil At Low Reynolds Numbers In The Langley Low Turbulence Pressure Tunnel

Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low turbulence Pressure Tunnel PDF
Author: Robert J. McGhee
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ISBN:
Size: 23.13 MB
Format: PDF, ePub, Mobi
Category : Aerofoils
Languages : en
Pages : 232
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Book Description:

Experimental Results For The Eppler 387 Airfoil At Low Reynolds Numbers In The Langley Low Turbulence Pressure Tunnel

Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low Turbulence Pressure Tunnel PDF
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723574788
Size: 62.22 MB
Format: PDF
Category :
Languages : en
Pages : 234
View: 7347

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Book Description: Experimental results were obtained for an Eppler 387 airfoil in the Langley Low Turbulence Pressure Tunnel. The tests were conducted over a Mach number range from 0.03 to 0.13 and a chord Reynolds number range for 60,000 to 460,000. Lift and pitching moment data were obtained from airfoil surface pressure measurements and drag data for wake surveys. Oil flow visualization was used to determine laminar separation and turbulent reattachment locations. Comparisons of these results with data on the Eppler 387 airfoil from two other facilities as well as the Eppler airfoil code are included. Mcghee, Robert J. and Walker, Betty S. and Millard, Betty F. Langley Research Center NASA-TM-4062, L-16430, NAS 1.15:4062 RTOP 505-60-21-01...

Experimental Results For The Eppler 387 Airfoil At Low Reynolds Numbers In The Langley Low Turbulence Pressure Tunnel

Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low turbulence Pressure Tunnel PDF
Author: Robert J. McGhee
Publisher:
ISBN:
Size: 21.71 MB
Format: PDF, ePub
Category : Aerofoils
Languages : en
Pages : 228
View: 3026

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Book Description: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)