词条 | Bagalini Bagaliante | |||||||||||||||||||
释义 |
The Bagalini Bagaliante (a portmanteau of "Bagalini" and "Glider") is an Italian high-wing, strut-braced, single-seat, pusher configuration, conventional landing gear motor glider that was designed by Marino Bagalini and made available as plans for amateur construction.[1][2] Design and developmentThe Bagaliante is constructed from wood and metal and is of pod-and-boom layout.[1] The {{convert|12.2|m|ft|1|abbr=on}} span wing employs a Göttingen 535 airfoil at the wing root, transitioning to an NACA 4412 section at the wingtip. The wing uses a semi-tapered planform, tapering outboard of the mid-span point. The specified engine is a {{convert|19|kW|hp|0|abbr=on}} Rotax 277 two-stroke aircraft engine, mounted aft of the cockpit and driving a pusher propeller mounted above the tail boom. The fixed mainwheels are located beside the fuselage on small sponsons.[1][3] Even with the small Rotax 277 fitted, the takeoff and landing distance is {{convert|46|m|ft|1|abbr=on}}[1] The estimated time to build the aircraft from the plans is 700 hours.[1] Specifications (Bagaliante){{Aircraft specs|ref=Purdy[1] |prime units?=met
See also{{aircontent|see also=
|related= |similar aircraft= |lists= }} References1. ^1 2 3 4 5 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 304. BAI Communications. {{ISBN|0-9636409-4-1}} 2. ^{{Cite web|url = http://www.pilotmix.com/index.php?pgid=11&lang=en&maxInfo=356|title = Bagalini Bagaliante|accessdate = 8 September 2011|last = Pilot Mix|authorlink = |year = n.d.}} 3. ^{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 8 September 2011|last = Lednicer |first = David |authorlink = |year = 2010}} External links
3 : Bagalini aircraft|Italian sailplanes 1980–1989|Homebuilt aircraft |
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