<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>Propeller-driven single-engine aircraft are affected by unsymmetrical flow of air around the fuse-lage, and especially around the vertical stabilizer [<xref ref-type="bibr" rid="j_tar-2018-0015_ref_001">1</xref>-<xref ref-type="bibr" rid="j_tar-2018-0015_ref_003">3</xref>]. This unsymmetrical, propeller-induced slip-stream produces sideslip [<xref ref-type="bibr" rid="j_tar-2018-0015_ref_004">4</xref>,<xref ref-type="bibr" rid="j_tar-2018-0015_ref_005">5</xref>] that needs to be compensated by the pilot using the rudder [<xref ref-type="bibr" rid="j_tar-2018-0015_ref_006">6</xref>]. In order to relieve the pilot from this additional task, automatic rudder deflection systems are used that compensate for sideslip by trimming the rudder accordingly. Such compensation algorithms are based on flight parameter measurements.</p>
<p>This paper presents more complex systems used to eliminate the phenomenon in question. In addition, it analyzes the existing solutions, based on patents divided into two groups. The first group deals with active slipstream effect compensation solutions, based on aircraft movement parameters that are derived from aircraft performance characteristics defined in advance. The other group comprises solutions that are based directly on feedback containing actual or estimated sideslip angle values. The most advanced systems rely on a combination of the two methods described above.</p>
</abstract>

Propeller-driven single-engine aircraft are affected by unsymmetrical flow of air around the fuse-lage, and especially around the vertical stabilizer [1-3]. This unsymmetrical, propeller-induced slip-stream produces sideslip [4,5] that needs to be compensated by the pilot using the rudder [6]. In order to relieve the pilot from this additional task, automatic rudder deflection systems are used that compensate for sideslip by trimming the rudder accordingly. Such compensation algorithms are based on flight parameter measurements.
This paper presents more complex systems used to eliminate the phenomenon in question. In addition, it analyzes the existing solutions, based on patents divided into two groups. The first group deals with active slipstream effect compensation solutions, based on aircraft movement parameters that are derived from aircraft performance characteristics defined in advance. The other group comprises solutions that are based directly on feedback containing actual or estimated sideslip angle values. The most advanced systems rely on a combination of the two methods described above.

Analysis of Methods Used to Eliminate the Propeller Slipstream Effect in Single-Engine Aircraft

Center of Space Technologies, Avionics Division

Transactions on Aerospace Research

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Propeller-driven single-engine aircraft are affected by unsymmetrical flow of air around the fuse-lage, and especially around the vertical stabilizer [1-3]....

Analysis of Methods Used to Eliminate the Propeller Slipstream Effect in Single-Engine Aircraft

Publié en ligne: 03 sept. 2019

Pages: 51 - 59

DOI: https://doi.org/10.2478/tar-2018-0015

Mots clés
single-engine aircraft, propeller slipstream, sideslip angle

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Analysis of Methods Used to Eliminate the Propeller Slipstream Effect in Single-Engine Aircraft

Publié en ligne: 03 sept. 2019

Pages: 51 - 59

DOI: https://doi.org/10.2478/tar-2018-0015

Mots cléssingle-engine aircraft, propeller slipstream, sideslip angle

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Mots clés
single-engine aircraft, propeller slipstream, sideslip angle