Performance Projections for a Helicopter Model with Plasma Actuators

Dor Polonsky; Oksana Stalnov; David Greenblatt

Performance Projections for a Helicopter Model with Plasma Actuators

Dor Polonsky, Oksana Stalnov, David Greenblatt

Research output: Contribution to conference › Paper › peer-review

Abstract

Dielectric barrier discharge actuators were evaluated for performance enhancement and noise reduction on the blades of a model helicopter. Results show that hover efficiency can be maintained or increased with increased rotor thrust. Simultaneously, broadband and tonal noise was significantly reduced. A system study, based on dimensional analysis, showed that a rotor diameter larger than approximately 1.5 meters is required to achieve an energetic break-even point.

Original language	English
State	Published - 2023
Event	62nd Israel Annual Conference on Aerospace Sciences, IACAS 2023 - Haifa, Israel Duration: 15 Mar 2023 → 16 Mar 2023

Conference

Conference	62nd Israel Annual Conference on Aerospace Sciences, IACAS 2023
Country/Territory	Israel
City	Haifa
Period	15/03/23 → 16/03/23

ASJC Scopus subject areas

Aerospace Engineering

Cite this

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title = "Performance Projections for a Helicopter Model with Plasma Actuators",

abstract = "Dielectric barrier discharge actuators were evaluated for performance enhancement and noise reduction on the blades of a model helicopter. Results show that hover efficiency can be maintained or increased with increased rotor thrust. Simultaneously, broadband and tonal noise was significantly reduced. A system study, based on dimensional analysis, showed that a rotor diameter larger than approximately 1.5 meters is required to achieve an energetic break-even point.",

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language = "אנגלית",

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T1 - Performance Projections for a Helicopter Model with Plasma Actuators

AU - Polonsky, Dor

AU - Stalnov, Oksana

AU - Greenblatt, David

PY - 2023

Y1 - 2023

N2 - Dielectric barrier discharge actuators were evaluated for performance enhancement and noise reduction on the blades of a model helicopter. Results show that hover efficiency can be maintained or increased with increased rotor thrust. Simultaneously, broadband and tonal noise was significantly reduced. A system study, based on dimensional analysis, showed that a rotor diameter larger than approximately 1.5 meters is required to achieve an energetic break-even point.

AB - Dielectric barrier discharge actuators were evaluated for performance enhancement and noise reduction on the blades of a model helicopter. Results show that hover efficiency can be maintained or increased with increased rotor thrust. Simultaneously, broadband and tonal noise was significantly reduced. A system study, based on dimensional analysis, showed that a rotor diameter larger than approximately 1.5 meters is required to achieve an energetic break-even point.

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T2 - 62nd Israel Annual Conference on Aerospace Sciences, IACAS 2023

Y2 - 15 March 2023 through 16 March 2023

ER -

Performance Projections for a Helicopter Model with Plasma Actuators

Abstract

Conference

ASJC Scopus subject areas

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