Characterization of Aeropropulsive Performance of Small Unmanned Aircraft System Paramotor.
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| Title: | Characterization of Aeropropulsive Performance of Small Unmanned Aircraft System Paramotor. |
|---|---|
| Authors: | Haefner, Alex C.1, Jones, Thomas L.2, Miller, Simon W.3, Cole, Julia A.4 |
| Source: | Journal of Aircraft. Jan/Feb2026, Vol. 63 Issue 1, p401-412. 12p. |
| Abstract: | A commercial-off-the-shelf small unmanned paramotor was analyzed through flight testing, computational aerodynamic simulation, and propulsion system modeling. Conventional flight-test procedures were adjusted to combat platform-specific challenges. Low-order modeling approaches were adapted for the vehicle and aeropropulsive performance characteristics of lift-to-drag ratio, climb rate, and power required for steady flight were verified. Having quantified the effect of wing loading on the aerodynamic performance of the vehicle, a process for estimating endurance as a function of payload weight and composition was developed and demonstrated. Results indicated that for the tested vehicle the maximum endurance was consistently found at the maximum manufacturer recommended flight weight. [ABSTRACT FROM AUTHOR] |
| Copyright of Journal of Aircraft is the property of American Institute of Aeronautics & Astronautics 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 |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 191758324 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Characterization of Aeropropulsive Performance of Small Unmanned Aircraft System Paramotor. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Haefner%2C+Alex+C%2E%22">Haefner, Alex C.</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Jones%2C+Thomas+L%2E%22">Jones, Thomas L.</searchLink><relatesTo>2</relatesTo><br /><searchLink fieldCode="AR" term="%22Miller%2C+Simon+W%2E%22">Miller, Simon W.</searchLink><relatesTo>3</relatesTo><br /><searchLink fieldCode="AR" term="%22Cole%2C+Julia+A%2E%22">Cole, Julia A.</searchLink><relatesTo>4</relatesTo> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Journal+of+Aircraft%22">Journal of Aircraft</searchLink>. Jan/Feb2026, Vol. 63 Issue 1, p401-412. 12p. – Name: Abstract Label: Abstract Group: Ab Data: A commercial-off-the-shelf small unmanned paramotor was analyzed through flight testing, computational aerodynamic simulation, and propulsion system modeling. Conventional flight-test procedures were adjusted to combat platform-specific challenges. Low-order modeling approaches were adapted for the vehicle and aeropropulsive performance characteristics of lift-to-drag ratio, climb rate, and power required for steady flight were verified. Having quantified the effect of wing loading on the aerodynamic performance of the vehicle, a process for estimating endurance as a function of payload weight and composition was developed and demonstrated. Results indicated that for the tested vehicle the maximum endurance was consistently found at the maximum manufacturer recommended flight weight. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Journal of Aircraft is the property of American Institute of Aeronautics & Astronautics 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.) |
| PLink | https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=191758324 |
| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.2514/1.C038360 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 12 StartPage: 401 Titles: – TitleFull: Characterization of Aeropropulsive Performance of Small Unmanned Aircraft System Paramotor. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Haefner, Alex C. – PersonEntity: Name: NameFull: Jones, Thomas L. – PersonEntity: Name: NameFull: Miller, Simon W. – PersonEntity: Name: NameFull: Cole, Julia A. IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 01 Text: Jan/Feb2026 Type: published Y: 2026 Identifiers: – Type: issn-print Value: 00218669 Numbering: – Type: volume Value: 63 – Type: issue Value: 1 Titles: – TitleFull: Journal of Aircraft Type: main |
| ResultId | 1 |
