Further Measurements of Model Propeller Pressure Distributions Using a Novel Technique

Further Measurements of Model Propeller Pressure Distributions Using a Novel Technique
Author: Stuart D. Jessup
Publisher:
Total Pages: 56
Release: 1986
Genre: Propellers
ISBN:

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Model propeller blade pressure distributions were measured using a novel technique. A single pressure gage was installed at a radial position to measure pressures at numerous chordwise locations through pressure taps and connecting channels. The technique resulted in accurate, detailed pressure distributions along two radial positions using two pressure gages. The major advantage of this technique is the ability to make measurements in the thin parts of the blade with high potential accuracy, and no disruption to the measuring surface, except for the orifice hole. The relatively along test time required to collect the data is the disadvantage. Keywords: Marine Propeller, Propeller Research Pressure Distribution, Model Experiments.


Further Measurements of Model Propeller Pressure Distributions Using a Novel Technique
Language: en
Pages: 56
Authors: Stuart D. Jessup
Categories: Propellers
Type: BOOK - Published: 1986 - Publisher:

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Model propeller blade pressure distributions were measured using a novel technique. A single pressure gage was installed at a radial position to measure pressur
Measurement of the Pressure Distribution on Two Model Propellers
Language: en
Pages: 227
Authors: Stuart D. Jessup
Categories: Propellers
Type: BOOK - Published: 1982 - Publisher:

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Measurement of the Pressure Distribution on Two Model Propellers
Language: en
Pages:
Authors:
Categories:
Type: BOOK - Published: 1982 - Publisher:

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Propellers/shafting '94 Symposium
Language: en
Pages: 404
Authors:
Categories: Propellers
Type: BOOK - Published: 1994 - Publisher:

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Advanced In-Flight Measurement Techniques
Language: en
Pages: 347
Authors: Fritz Boden
Categories: Technology & Engineering
Type: BOOK - Published: 2013-02-13 - Publisher: Springer Science & Business Media

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The book presents a synopsis of the main results achieved during the 3 year EU-project "Advanced Inflight Measurement Techniques (AIM)" which applied advanced i