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Nasa Technical Reports Server (ntrs) 20090019125%3a The Effect Of Lateral Inclination Of The Thrust Axis And Of Sweepback Of The Leading Edge Of The Wing On Propulsive And Net Efficiencies Of A Wing Nacelle Propeller Combination by Nasa Technical Reports Server (ntrs)
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1NASA Technical Reports Server (NTRS) 20090019125: The Effect Of Lateral Inclination Of The Thrust Axis And Of Sweepback Of The Leading Edge Of The Wing On Propulsive And Net Efficiencies Of A Wing-Nacelle-Propeller Combination
By NASA Technical Reports Server (NTRS)
This report describes and gives the results of tests made to determine the effect of lateral inclination of the propeller thrust axis to the direction of flight. A wing-nacelle-propeller combination with the nacelle axis located successively parallel to and at 15 degrees to the perpendicular to the leading edge of a wing was tested with the combination at several angles of yaw. Tests of the wing alone at the same angles of yaw were also made. The data are presented in the usual graphic form. An increase in propulsive efficiency with increase in angle of the thrust axis was found. The change in net efficiency, found by charging the whole nacelle drag to the power unit, was negligible, however, within the range of the tests.
“NASA Technical Reports Server (NTRS) 20090019125: The Effect Of Lateral Inclination Of The Thrust Axis And Of Sweepback Of The Leading Edge Of The Wing On Propulsive And Net Efficiencies Of A Wing-Nacelle-Propeller Combination” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20090019125: The Effect Of Lateral Inclination Of The Thrust Axis And Of Sweepback Of The Leading Edge Of The Wing On Propulsive And Net Efficiencies Of A Wing-Nacelle-Propeller Combination
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_20090019125
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The book is available for download in "texts" format, the size of the file-s is: 17.58 Mbs, the file-s for this book were downloaded 95 times, the file-s went public at Sun Jan 18 2015.
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