1915
DOI: 10.1111/j.1559-3584.1915.tb00408.x
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A Contribution to the Theory of Propulsion and the Screw Propeller

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Cited by 76 publications
(65 citation statements)
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“…From 1910 to 1915 there was a lively discussion on both Froude's and Parsons' theories between professors Henderson, Froude, Parsons and Lanchester in the pages of the popular English publication "Transactions of the Institute of Naval Architects" (see issues of 52, 53, 55 and 56). The author of the last article was Lanchester [28]. In the introduction to this article, he wrote: -"The present investigation takes for its starting point the simplified or idealized conception of propeller due to Mr. R.E.…”
Section: The Creation Of the Actuator Disc Theorymentioning
confidence: 99%
See 1 more Smart Citation
“…From 1910 to 1915 there was a lively discussion on both Froude's and Parsons' theories between professors Henderson, Froude, Parsons and Lanchester in the pages of the popular English publication "Transactions of the Institute of Naval Architects" (see issues of 52, 53, 55 and 56). The author of the last article was Lanchester [28]. In the introduction to this article, he wrote: -"The present investigation takes for its starting point the simplified or idealized conception of propeller due to Mr. R.E.…”
Section: The Creation Of the Actuator Disc Theorymentioning
confidence: 99%
“…3 which was reproduced from Fig. 6 of [28] where Q is a measure (ratio) of the ideal work done by the force field and the energy in the wake, which according to Lanchester may not be equal).…”
Section: The Creation Of the Actuator Disc Theorymentioning
confidence: 99%
“…The linear momentum actuator disc theory often referred to as momentum theory or actuator disc theory was first introduced by Rankine [14] and Froude [15] to model ship propellers and subsequently extended by Lanchester [33] and Betz [34], who derived limits on the efficiency for this model. More recently, the theory has been particularised to model helicopter rotors [35], centrifugal pumps, turbochargers and wind turbines [36].…”
Section: Turbine Modellingmentioning
confidence: 99%
“…This is a basic principle that is easy to visualize: The complete extraction of kinetic energy from the flow would reduce the current speed to zero, thus leaving motionless water on the downstream side of the blade circle, which would prevent further flow through the turbine. The theoretical maximum fraction of kinetic energy flowing through a blade circle that can be extracted by the rotor is 59%-the well-known Lanchester-Betz limit, commonly referred to as the Betz limit (Lanchester 1915, Betz 1920, Van Kuik 2007. A real turbine will extract an even smaller fraction than this because of friction, turbulence, wake generation, possible cavitation, vibration of the rotor/generator assembly, and so on.…”
Section: Extracting Marine Hydrokinetic Energymentioning
confidence: 99%