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Power optimization of a single propeller airplane take-off run on the basis of lateral maneuver limitations.

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Title: Power optimization of a single propeller airplane take-off run on the basis of lateral maneuver limitations.
Authors: Stojaković, Predrag1, Velimirović, Kosta1, Rašuo, Boško2 brasuo@mas.bg.ac.rs
Source: Aerospace Science & Technology. Jan2018, Vol. 72, p553-563. 11p.
Subjects: Propeller-driven aircraft, Airplane maneuverability, Airspeed airplanes, Airplane takeoff, Runways (Aeronautics)
Abstract: The problem of selecting optimal take-off run power of a single propeller airplane on the basis of the lateral maneuver limitations is analyzed in this paper. The single propeller reactive torque as the function of engine power and speed generates non-aerodynamic asymmetric load disturbance. The capability of lateral flight control surfaces to compensate for this asymmetric load and perform the required maneuver defines the safe flight envelope boundaries in the form of engine power setting – airspeed relation. The take-off run length consisting of acceleration, decision making, brake activation and airplane stopping length distances is calculated for engine power settings along the safe flight boundaries defined by the lateral flight control capabilities. The minimum of take-off run along thus defined safe flight boundary determines the engine optimal power setting. The results are presented for the example of the single propeller airplane on concrete runway surface. [ABSTRACT FROM AUTHOR]
Copyright of Aerospace Science & Technology is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
Database: Engineering Source
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Header DbId: egs
DbLabel: Engineering Source
An: 126898234
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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  Data: Power optimization of a single propeller airplane take-off run on the basis of lateral maneuver limitations.
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  Data: <searchLink fieldCode="AR" term="%22Stojaković%2C+Predrag%22">Stojaković, Predrag</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Velimirović%2C+Kosta%22">Velimirović, Kosta</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Rašuo%2C+Boško%22">Rašuo, Boško</searchLink><relatesTo>2</relatesTo><i> brasuo@mas.bg.ac.rs</i>
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  Data: <searchLink fieldCode="JN" term="%22Aerospace+Science+%26+Technology%22">Aerospace Science & Technology</searchLink>. Jan2018, Vol. 72, p553-563. 11p.
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  Data: <searchLink fieldCode="DE" term="%22Propeller-driven+aircraft%22">Propeller-driven aircraft</searchLink><br /><searchLink fieldCode="DE" term="%22Airplane+maneuverability%22">Airplane maneuverability</searchLink><br /><searchLink fieldCode="DE" term="%22Airspeed+airplanes%22">Airspeed airplanes</searchLink><br /><searchLink fieldCode="DE" term="%22Airplane+takeoff%22">Airplane takeoff</searchLink><br /><searchLink fieldCode="DE" term="%22Runways+%28Aeronautics%29%22">Runways (Aeronautics)</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: The problem of selecting optimal take-off run power of a single propeller airplane on the basis of the lateral maneuver limitations is analyzed in this paper. The single propeller reactive torque as the function of engine power and speed generates non-aerodynamic asymmetric load disturbance. The capability of lateral flight control surfaces to compensate for this asymmetric load and perform the required maneuver defines the safe flight envelope boundaries in the form of engine power setting – airspeed relation. The take-off run length consisting of acceleration, decision making, brake activation and airplane stopping length distances is calculated for engine power settings along the safe flight boundaries defined by the lateral flight control capabilities. The minimum of take-off run along thus defined safe flight boundary determines the engine optimal power setting. The results are presented for the example of the single propeller airplane on concrete runway surface. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Aerospace Science & Technology is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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      – Type: doi
        Value: 10.1016/j.ast.2017.10.015
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      – Code: eng
        Text: English
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      Pagination:
        PageCount: 11
        StartPage: 553
    Subjects:
      – SubjectFull: Propeller-driven aircraft
        Type: general
      – SubjectFull: Airplane maneuverability
        Type: general
      – SubjectFull: Airspeed airplanes
        Type: general
      – SubjectFull: Airplane takeoff
        Type: general
      – SubjectFull: Runways (Aeronautics)
        Type: general
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      – TitleFull: Power optimization of a single propeller airplane take-off run on the basis of lateral maneuver limitations.
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              Text: Jan2018
              Type: published
              Y: 2018
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