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Proceedings Paper

Application of pressure sensitive paint for determination of aerodynamic loads and moments on propeller blade
Author(s): V. P. Kulesh; V. E. Mosharov; A. A. Orlov; S. P. Ostroukhov; V. N. Radchenko
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Paper Abstract

Specific features of application of Pressure Sensitive Paint (PSP) method for propeller blades investigation are discussed. Pressure fields on both sides of the blade of twin-blade propeller model were measured by PSP. The model was investigated at rotation rates up to 5300 rpm at blades pitch angles 15°, 35° and 45° without external airflow. Propeller thrust, torque and blade pitch moment were calculated. Thrust and torque were also measured by balance. Good agreement between PSP and balance results can confirm the reliability of PSP measurements on propellers.

Paper Details

Date Published: 10 June 2006
PDF: 8 pages
Proc. SPIE 6262, Optical Methods of Flow Investigation, 62620K (10 June 2006); doi: 10.1117/12.683025
Show Author Affiliations
V. P. Kulesh, Central Aero-Hydrodynamic Institute (Russia)
V. E. Mosharov, Central Aero-Hydrodynamic Institute (Russia)
A. A. Orlov, Central Aero-Hydrodynamic Institute (Russia)
S. P. Ostroukhov, Central Aero-Hydrodynamic Institute (Russia)
V. N. Radchenko, Central Aero-Hydrodynamic Institute (Russia)


Published in SPIE Proceedings Vol. 6262:
Optical Methods of Flow Investigation
Yuri N. Dubnistchev; Bronyus S. Rinkevichyus, Editor(s)

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