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Longitudinal stability characteristics of the LASTA airplane.

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Title: Longitudinal stability characteristics of the LASTA airplane.
Authors: Milenković-Babić, Miodrag1 miodragmbm@yahoo.co.uk, Samardžić, Marija1 majasam@ptt.rs, Antonić, Vuk1 vukantonic@gmail.com, Marjanović, Milica1 milicagoran@gmail.com, Stefanović-Gobeljić, Vanja1 vanja_stef@yahoo.com
Source: Aircraft Engineering & Aerospace Technology. 2017, Vol. 89 Issue 6, p911-919. 9p.
Subjects: Propeller-driven aircraft, Airplane control systems, Longitudinal method, Aerodynamics, Flight testing of airplanes
Abstract: Purpose This paper presents the longitudinal stability analysis of a single tractor propeller airplane LASTA at high engine power settings. This analysis is part of the ongoing process of certifying the airplane for civil use according to the civil regulations CS-23.Design/methodology/approach The design methodology that is presented in the paper consists of comparing flight test aerodynamic and calculation results. The methods used here are standard and routinely used in flight testing.Findings Flight testing results indicate that at low airspeeds the cumulative destabilizing effects because of high values of the angle of attack and high power settings are about 6 per cent of MAC. This value is in a very good agreement with published data.Practical implications The information presented in this paper are new, and are very specific to this one aircraft configuration. The methods used here are standard and widely used in flight testing.Originality/value The information in this paper presents flight test results. There are not many publications in this area. [ABSTRACT FROM AUTHOR]
Copyright of Aircraft Engineering & Aerospace Technology is the property of Emerald Publishing Limited 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: 126142074
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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Items – Name: Title
  Label: Title
  Group: Ti
  Data: Longitudinal stability characteristics of the LASTA airplane.
– Name: Author
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  Data: <searchLink fieldCode="AR" term="%22Milenković-Babić%2C+Miodrag%22">Milenković-Babić, Miodrag</searchLink><relatesTo>1</relatesTo><i> miodragmbm@yahoo.co.uk</i><br /><searchLink fieldCode="AR" term="%22Samardžić%2C+Marija%22">Samardžić, Marija</searchLink><relatesTo>1</relatesTo><i> majasam@ptt.rs</i><br /><searchLink fieldCode="AR" term="%22Antonić%2C+Vuk%22">Antonić, Vuk</searchLink><relatesTo>1</relatesTo><i> vukantonic@gmail.com</i><br /><searchLink fieldCode="AR" term="%22Marjanović%2C+Milica%22">Marjanović, Milica</searchLink><relatesTo>1</relatesTo><i> milicagoran@gmail.com</i><br /><searchLink fieldCode="AR" term="%22Stefanović-Gobeljić%2C+Vanja%22">Stefanović-Gobeljić, Vanja</searchLink><relatesTo>1</relatesTo><i> vanja_stef@yahoo.com</i>
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  Data: <searchLink fieldCode="JN" term="%22Aircraft+Engineering+%26+Aerospace+Technology%22">Aircraft Engineering & Aerospace Technology</searchLink>. 2017, Vol. 89 Issue 6, p911-919. 9p.
– Name: Subject
  Label: Subjects
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  Data: <searchLink fieldCode="DE" term="%22Propeller-driven+aircraft%22">Propeller-driven aircraft</searchLink><br /><searchLink fieldCode="DE" term="%22Airplane+control+systems%22">Airplane control systems</searchLink><br /><searchLink fieldCode="DE" term="%22Longitudinal+method%22">Longitudinal method</searchLink><br /><searchLink fieldCode="DE" term="%22Aerodynamics%22">Aerodynamics</searchLink><br /><searchLink fieldCode="DE" term="%22Flight+testing+of+airplanes%22">Flight testing of airplanes</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: Purpose This paper presents the longitudinal stability analysis of a single tractor propeller airplane LASTA at high engine power settings. This analysis is part of the ongoing process of certifying the airplane for civil use according to the civil regulations CS-23.Design/methodology/approach The design methodology that is presented in the paper consists of comparing flight test aerodynamic and calculation results. The methods used here are standard and routinely used in flight testing.Findings Flight testing results indicate that at low airspeeds the cumulative destabilizing effects because of high values of the angle of attack and high power settings are about 6 per cent of MAC. This value is in a very good agreement with published data.Practical implications The information presented in this paper are new, and are very specific to this one aircraft configuration. The methods used here are standard and widely used in flight testing.Originality/value The information in this paper presents flight test results. There are not many publications in this area. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Aircraft Engineering & Aerospace Technology is the property of Emerald Publishing Limited 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: 10.1108/AEAT-02-2016-0026
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      – Code: eng
        Text: English
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        PageCount: 9
        StartPage: 911
    Subjects:
      – SubjectFull: Propeller-driven aircraft
        Type: general
      – SubjectFull: Airplane control systems
        Type: general
      – SubjectFull: Longitudinal method
        Type: general
      – SubjectFull: Aerodynamics
        Type: general
      – SubjectFull: Flight testing of airplanes
        Type: general
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      – TitleFull: Longitudinal stability characteristics of the LASTA airplane.
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            NameFull: Milenković-Babić, Miodrag
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            NameFull: Antonić, Vuk
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            NameFull: Stefanović-Gobeljić, Vanja
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              Text: 2017
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