This HTML5 document contains 108 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
dctermshttp://purl.org/dc/terms/
dbohttp://dbpedia.org/ontology/
n17http://dbpedia.org/resource/File:
foafhttp://xmlns.com/foaf/0.1/
n13http://dbpedia.org/property/wingLoadingKg/
n19https://global.dbpedia.org/id/
schemahttp://schema.org/
dbthttp://dbpedia.org/resource/Template:
rdfshttp://www.w3.org/2000/01/rdf-schema#
n11http://commons.wikimedia.org/wiki/Special:FilePath/
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
owlhttp://www.w3.org/2002/07/owl#
wikipedia-enhttp://en.wikipedia.org/wiki/
dbchttp://dbpedia.org/resource/Category:
dbphttp://dbpedia.org/property/
provhttp://www.w3.org/ns/prov#
xsdhhttp://www.w3.org/2001/XMLSchema#
wikidatahttp://www.wikidata.org/entity/
goldhttp://purl.org/linguistics/gold/
dbrhttp://dbpedia.org/resource/

Statements

Subject Item
dbr:Schmeidler_SN.2
rdf:type
wikidata:Q11436 dbo:Aircraft dbo:BasketballPlayer schema:Product owl:Thing dbo:MeanOfTransportation
rdfs:label
Schmeidler SN.2
rdfs:comment
The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty.
foaf:depiction
n11:Schmeidler_SN.2_L'Aerophile_February_1933.jpg n11:Schmeidler_SN.2_3-view_L'Aerophile_February_1933.jpg
dcterms:subject
dbc:Variable-geometry-wing_aircraft dbc:High-wing_aircraft dbc:1930s_German_experimental_aircraft dbc:Aircraft_first_flown_in_1932 dbc:Single-engined_tractor_aircraft
dbo:wikiPageID
48755543
dbo:wikiPageRevisionID
1109638556
dbo:wikiPageWikiLink
dbr:Fin dbr:Breslau dbr:Flap_(aeronautics) dbc:High-wing_aircraft dbr:Germany dbr:Elevator_(aeronautics) dbr:Monoplane dbc:1930s_German_experimental_aircraft dbr:Rack_and_pinion dbr:Tailplane dbr:Wolf_Hirth dbr:Rudder dbr:Makhonine_Mak-10 dbr:Lift_coefficient dbr:Empennage dbr:Shock_absorber n17:Schmeidler_SN.2_3-view_L'Aerophile_February_1933.jpg dbr:BMW_X dbr:Berlin dbr:Balanced_rudder dbr:Leading_edge dbc:Aircraft_first_flown_in_1932 dbr:Airfoil dbr:Leading_edge_slot dbr:Werner_Schmeidler dbr:Strut dbr:Drag_(aerodynamics) dbr:Cantilever dbr:Trailing_edge dbr:Tempelhof dbr:Aileron dbr:Radial_engine dbr:Wrocław_University_of_Technology dbr:Camber_(aeronautics) dbr:High_wing dbc:Variable-geometry-wing_aircraft dbr:Chord_(aeronautics) dbc:Single-engined_tractor_aircraft
owl:sameAs
wikidata:Q22115631 n19:26K3P
dbp:spanM
11.4
dbp:wingAreaNote
maximum,
dbp:wingAreaSqm
12.75
n13:m
42.5
dbp:wingLoadingNote
wing extensions retracted :::: wing extensions extended
dbp:wikiPageUsesTemplate
dbt:Cvt dbt:Reflist dbt:Convert dbt:Infobox_aircraft_type dbt:Aircraft_specs
dbo:thumbnail
n11:Schmeidler_SN.2_L'Aerophile_February_1933.jpg?width=300
dbp:primeUnits%3F_
met
dbp:firstFlight
1932-01-12
dbp:nationalOrigin
dbr:Germany
dbp:crew
1
dbp:designer
Werner Schmeidler, Neumann
dbp:fuelCapacity
fuel ; oil
dbp:manufacturer
dbr:Wrocław_University_of_Technology
dbp:ref
General: L'Aérophile February 1933 Performance: Flugsport March 1932, Flugzeug-Typenbuch 1944
dbp:type
Experimental variable wing area aircraft
dbo:abstract
The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty.
dbp:airfoil
Göttingen 387
dbp:ceilingM
2930
dbp:ceilingNote
wing extensions retracted :::: wing extensions extended
dbp:climbRateMs
1.7
dbp:climbRateNote
wing extensions retracted :::: wing extensions extended
dbp:emptyWeightKg
355
dbp:emptyWeightNote
equipped
dbp:endurance
7200.0
dbp:eng1Name
dbr:BMW_X
dbp:eng1Number
1
dbp:eng1Type
five cylinder radial
dbp:grossWeightKg
470
dbp:heightM
2
dbp:lengthM
6.2
dbp:maxSpeedKmh
160
dbp:maxSpeedNote
wing extensions retracted :::: wing extensions extended *Take-off speed: *Landing speed: wing extensions retracted :::: wing extensions extended
dbp:morePerformance
*Take-off distance into wind, minimum wing extension: *Take-off distance into wind, maximum wing extension: *Landing run, minimum wing extension: *Landing run, maximum wing extension:
dbp:numberBuilt
1
dbp:propBladeNumber
2
dbp:propDiaM
1.9
dbp:propName
metal fixed-pitch propeller
dbp:rangeKm
300
gold:hypernym
dbr:Power
prov:wasDerivedFrom
wikipedia-en:Schmeidler_SN.2?oldid=1109638556&ns=0
dbo:wikiPageLength
10957
dbo:numberBuilt
1
dbo:designer
dbr:Werner_Schmeidler
dbo:manufacturer
dbr:Wrocław_University_of_Technology
dbo:origin
dbr:Germany
foaf:isPrimaryTopicOf
wikipedia-en:Schmeidler_SN.2