About: De Havilland DH.52     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon
http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FDe_Havilland_DH.52

The de Havilland DH.52 was a single-seat, high-winged glider produced as an entrant to a 1922 prize competition. Two were built but insufficient torsional stiffness in the wings led to control problems and the DH.52 was rapidly abandoned.

AttributesValues
rdf:type
rdfs:label
  • De Havilland DH.52 (en)
  • De Havilland DH.52 (it)
rdfs:comment
  • The de Havilland DH.52 was a single-seat, high-winged glider produced as an entrant to a 1922 prize competition. Two were built but insufficient torsional stiffness in the wings led to control problems and the DH.52 was rapidly abandoned. (en)
  • Il de Havilland DH.52 fu un aliante monoposto ad ala alta realizzato per partecipare ad una gara svoltasi nel 1922. Furono costruiti solo due esemplari e poi il progetto venne abbandonato per via di problemi di rigidità torsionale delle ali, che causavano problemi di controllo del velivolo. (it)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/DH52SideDraw.png
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
span m
stall speed kmh
wing area sqm
wing loading kg/m
dbp:wikiPageUsesTemplate
thumbnail
dbp:primeUnits%3F_
  • imp (en)
first flight
national origin
  • United Kingdom (en)
crew
manufacturer
retired
type
  • single seat glider (en)
has abstract
  • The de Havilland DH.52 was a single-seat, high-winged glider produced as an entrant to a 1922 prize competition. Two were built but insufficient torsional stiffness in the wings led to control problems and the DH.52 was rapidly abandoned. (en)
  • Il de Havilland DH.52 fu un aliante monoposto ad ala alta realizzato per partecipare ad una gara svoltasi nel 1922. Furono costruiti solo due esemplari e poi il progetto venne abbandonato per via di problemi di rigidità torsionale delle ali, che causavano problemi di controllo del velivolo. (it)
airfoil
aspect ratio
empty weight kg
gross weight kg
length m
number built
gold:hypernym
prov:wasDerivedFrom
page length (characters) of wiki page
number built
retired
manufacturer
foaf:isPrimaryTopicOf
is Link from a Wikipage to another Wikipage of
is foaf:primaryTopic of
Faceted Search & Find service v1.17_git139 as of Feb 29 2024


Alternative Linked Data Documents: ODE     Content Formats:   [cxml] [csv]     RDF   [text] [turtle] [ld+json] [rdf+json] [rdf+xml]     ODATA   [atom+xml] [odata+json]     Microdata   [microdata+json] [html]    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 60 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software