About: Weber-Landholf-Münch WLM-1

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About: Weber-Landholf-Münch WLM-1 Goto Sponge NotDistinct Permalink

An Entity of Type : dbo:Aircraft, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FWeber-Landholf-Münch_WLM-1&invfp=IFP_OFF&sas=SAME_AS_OFF

The Weber-Landholf-Münch WLM-1 is a 1940s Swiss high performance sailplane designed to meet a Swiss Air Force (SAF) requirement for a training glider that could initiate potential fighter pilots. To this end it is fast, aerobatic and equipped with standard military instrumentation. Only three were built.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Weber-Landholf-Münch WLM-1 (en)
rdfs:comment	The Weber-Landholf-Münch WLM-1 is a 1940s Swiss high performance sailplane designed to meet a Swiss Air Force (SAF) requirement for a training glider that could initiate potential fighter pilots. To this end it is fast, aerobatic and equipped with standard military instrumentation. Only three were built. (en)
dcterms:subject	High-wing aircraft Aircraft first flown in 1946 1940s Swiss military trainer aircraft 1940s Swiss sailplanes
Wikipage page ID	61191762 (xsd:integer)
Wikipage revision ID	1101092288 (xsd:integer)
Link from a Wikipage to another Wikipage	Samedan Elevator (aeronautics) De Havilland Vampire Sailplane Thickness-to-chord ratio Lupfig Plywood Spar (aeronautics) Leading edge Aerobatic Ailerons High-wing aircraft Fin Balanced rudder Glider (sailplane) Trailing edge Aircraft first flown in 1946 Aeroelastic flutter Swiss Air Force Switzerland 1940s Swiss military trainer aircraft 1940s Swiss sailplanes Tailplane Dihedral (aeronautics) Spoiler (aeronautics) Rudder Flap (aeronautics) High wing Canopy (aeronautics) Spin (aeronautics)
sameAs	Weber-Landholf-Münch WLM-1 Weber-Landholf-Münch WLM-1
sink rate ms	0.800000 (xsd:double)
sink rate note	minimum, with 10° flap and at (en)
span m	14 (xsd:integer)
stall speed kmh	46 (xsd:integer)
stall speed note	minimum, with full, 40° flap (en)
wing area sqm	14 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cn dbt:Cvt dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	1947-07-21 (xsd:date)
national origin	Switzerland
crew	One (en)
designer	Rudolf Sägesser (en)
manufacturer	Isler & Co., Wildegg (en)
ref	The World's Sailplanes (en)
type	High performance training and racing glider (en)
has abstract	The Weber-Landholf-Münch WLM-1 is a 1940s Swiss high performance sailplane designed to meet a Swiss Air Force (SAF) requirement for a training glider that could initiate potential fighter pilots. To this end it is fast, aerobatic and equipped with standard military instrumentation. Only three were built. (en)
airfoil	NACA 23013 at root to NACA 23007 tip (en)
aspect ratio	14 (xsd:integer)
empty weight kg	210 (xsd:integer)
glide ratio	25 (xsd:integer)
gross weight kg	310 (xsd:integer)
length m	7 (xsd:integer)
max speed kmh	300 (xsd:integer)
max speed note	placard, smooth air (en)
number built	3 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:Weber-Landholf-Münch_WLM-1?oldid=1101092288&ns=0
page length (characters) of wiki page	7241 (xsd:nonNegativeInteger)
number built	3 (xsd:nonNegativeInteger)
origin	Switzerland
type	Glider (sailplane)
foaf:isPrimaryTopicOf	wikipedia-en:Weber-Landholf-Münch_WLM-1
is Link from a Wikipage to another Wikipage of	List of gliders (W)
is foaf:primaryTopic of	wikipedia-en:Weber-Landholf-Münch_WLM-1

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