About: Bede XBD-2

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The Bede XBD-2 was an experimental short takeoff and landing (STOL) aircraft, with several novel features such as structural use of glass-fibre and aluminium honeycomb, a suction boundary layer control (BLC) system and fuselage-mounted twin engines driving a pusher configuration, shrouded single propeller. The sole example flew in the early 1960s in the United States.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Bede XBD-2 (en) Bede XBD-2 (fr)
rdfs:comment	The Bede XBD-2 was an experimental short takeoff and landing (STOL) aircraft, with several novel features such as structural use of glass-fibre and aluminium honeycomb, a suction boundary layer control (BLC) system and fuselage-mounted twin engines driving a pusher configuration, shrouded single propeller. The sole example flew in the early 1960s in the United States. (en) Le Bede XBD-2 est un avion expérimental américain destiné à tester les effets du contrôle de la couche limite sur la portance, en particulier à basse vitesse. (fr)
differentFrom	Bede BD-2
dcterms:subject	Bede aircraft Low-wing aircraft Aircraft first flown in 1961 Ducted fan-powered aircraft 1960s United States experimental aircraft Twin-engined single-prop pusher aircraft
Wikipage page ID	35742708 (xsd:integer)
Wikipage revision ID	1108912505 (xsd:integer)
Link from a Wikipage to another Wikipage	Bede aircraft Bede Aircraft Bede BD-3 University of Maryland, College Park Elevator (aircraft) Continental O-300 Sprag clutch Boundary layer control Camber (aerodynamics) Polyurethane STOL Low-wing aircraft Aileron Aircraft first flown in 1961 Ducted fan-powered aircraft Fuselage Leading edge Fin Trailing edge Propeller Pusher configuration 1960s United States experimental aircraft Twin-engined single-prop pusher aircraft Tailplane Manitowoc County, Wisconsin Fairing (aircraft) Aspect ratio (wing) Cantilever Rudder Experimental aircraft Dihedral (aircraft) Flat-six engine Tricycle undercarriage Piston engine Horizontally opposed Glass-fibre
Link from a Wikipage to an external page
sameAs	Bede XBD-2 Bede XBD-2 Bede XBD-2 Bede XBD-2 Bede XBD-2
span m	11.420000 (xsd:double)
stall speed mph	42 (xsd:integer)
stall speed note	with BLC. Without BLC 64 mph (en)
wing area sqm	13.940000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Distinguish dbt:Reflist dbt:Bede_aircraft dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	imp (en)
first flight	1961-07-26 (xsd:date)
national origin	United States (en)
capacity	four total (en)
crew	one (en)
manufacturer	Bede Aircraft
ref	Jane's All the World's Aircraft 1962-63 (en)
type	Experimental aircraft
has abstract	The Bede XBD-2 was an experimental short takeoff and landing (STOL) aircraft, with several novel features such as structural use of glass-fibre and aluminium honeycomb, a suction boundary layer control (BLC) system and fuselage-mounted twin engines driving a pusher configuration, shrouded single propeller. The sole example flew in the early 1960s in the United States. (en) Le Bede XBD-2 est un avion expérimental américain destiné à tester les effets du contrôle de la couche limite sur la portance, en particulier à basse vitesse. (fr)
airfoil	Göttingen 549 (en)
ceiling ft	21000 (xsd:integer)
ceiling note	service (en)
climb rate ftmin	1050 (xsd:integer)
cruise speed mph	179 (xsd:integer)
cruise speed note	maximum at 65% power at 9,000ft (en)
developed into	Bede BD-3
eng1 hp	145 (xsd:integer)
eng1 name	Continental O-300-A (en)
eng1 number	2 (xsd:integer)
eng1 type	6 (xsd:integer)

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