Arnold AR-5

{{Short description|Aircraft Model}}

File:AR-5_Sport_Monoplane,_designed_and_built_by_Mike_Arnold,_1992_-_Hiller_Aviation_Museum_-_San_Carlos,_California_-_DSC03250.jpg

The Arnold AR-5 is an experimental single seat, low-wing sport monoplane with fixed conventional undercarriage, designed and built by Mike Arnold.

Development and design

Originally conceived by Mike Arnold as a personal sport airplane with excellent performance and good handling qualities. The design outperformed initial performance estimates for its relatively low power output, exceeding 200mph with only 65hp.{{Cite web|date=2016-10-20|title=Prologue - Mike Arnold and the AR-5|url=http://www.ar-5.com/images/sportsmanpilot1.PDF|url-status=live|access-date=2021-11-22|archive-url=https://web.archive.org/web/20161020013923/http://www.ar-5.com/images/sportsmanpilot1.PDF|archive-date=2016-10-20}} Constructed of fiberglass-epoxy matrix composite material utilizing the "moldless method" popularized by Burt Rutan.{{Cite book|last=Factory|first=Rutan Aircraft|url=https://books.google.com/books?id=eRyiMwAACAAJ|title=Moldless Composite Sandwich Aircraft Construction|date=2005|publisher=Aircraft Technical Book Company|isbn=978-0-9774896-1-9|language=en|access-date=2021-11-22|archive-date=2022-03-04|archive-url=https://web.archive.org/web/20220304214310/https://books.google.com/books?id=eRyiMwAACAAJ|url-status=live}} Careful attention to aerodynamic detail resulted in noteworthy laminar flow drag reduction, as documented by aerodynamicists Alex Strojnik and Bruce Carmichael.{{cn|date=September 2023}}

Legacy

In 1992, the AR-5 flown by Mike Arnold set the FAI C1a Class World Speed Record of 343,08 km/h over a 3.0km course.{{Cite web|date=2017-10-10|title=Michael S. Arnold (USA) (1097)|url=https://www.fai.org/record/1097|access-date=2021-11-22|website=www.fai.org|language=en|archive-date=2021-11-22|archive-url=https://web.archive.org/web/20211122111853/https://www.fai.org/record/1097|url-status=live}} Mike wrote several articles about his design methodology for various magazines.{{Cite web|title="Inverse Pressure. Gradient Matching ... and other ideas for designing fast, low wing airplanes that climb and turn like mad" by MIKE ARNOLD|url=http://contrails.free.fr/temp/Inverse%20pressure%20gradient%20matching.pdf|url-status=live|access-date=2021-11-22|archive-date=2015-09-30|archive-url=https://web.archive.org/web/20150930143312/http://contrails.free.fr/temp/Inverse%20pressure%20gradient%20matching.pdf}}{{Cite web|last=Kitplanes|date=2021-07-02|title=Archive: October 1999|url=https://www.kitplanes.com/archive-october-1999/|access-date=2021-11-22|website=KITPLANES|language=en-US|archive-date=2021-11-22|archive-url=https://web.archive.org/web/20211122111854/https://www.kitplanes.com/archive-october-1999/|url-status=live}} The sole existing example resides at the Hiller Aviation Museum, San Carlos, CA.{{Cite web|title=Hiller Aviation Museum - Models on Display|url=https://www.hiller.org/museum/aircraft-on-display/|url-status=live|access-date=2021-11-22|website=Hiller Aviation Museum|language=en-US|archive-date=2021-11-22|archive-url=https://web.archive.org/web/20211122111856/https://www.hiller.org/museum/aircraft-on-display/}}

Specifications

{{Aircraft specs|prime units?=imp|airfoil note=Tip: NACA 65/2-215|range note=45 min reserve|range miles=500|eng1 type=Inline, Liquid Cooled 2-Stroke.|fuel capacity=12 Gal|wing area sqft=55.125|aspect ratio=8|airfoil=Root: NACA 65/3-418|span ft=21|eng1 hp=65|eng1 name=Rotax 582|empty weight lb=488|stall speed mph=53|cruise speed mph=207|max speed mph=213.18|g limits=+6/-4g|max speed note=}}

References

{{reflist|30em}}

Category:Racing aircraft