View as:
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RDF/XML
<rdf:RDF
xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#"
xmlns:j.0="http://qudt.org/schema/qudt/"
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xmlns:j.2="http://www.w3.org/2004/02/skos/core#"
xmlns:rdfs="http://www.w3.org/2000/01/rdf-schema#"
xmlns:xsd="http://www.w3.org/2001/XMLSchema#" >
<rdf:Description rdf:about="http://qudt.org/vocab/quantitykind/Thrust">
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloLB_F"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/N"/>
<j.2:broader rdf:resource="http://qudt.org/vocab/quantitykind/Force"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloGM_F"/>
<j.1:description rdf:datatype="http://qudt.org/schema/qudt/LatexString">Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.
The pushing or pulling force developed by an aircraft engine or a rocket engine.
The force exerted in any direction by a fluid jet or by a powered screw, as, the thrust of an antitorque rotor.
Specifically, in rocketry, $ F\,= m\cdot v$ where m is propellant mass flow and v is exhaust velocity relative to the vehicle. Also called momentum thrust.</j.1:description>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloN"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiN"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroN"/>
<j.0:dbpediaMatch rdf:datatype="http://www.w3.org/2001/XMLSchema#anyURI">http://dbpedia.org/resource/Thrust</j.0:dbpediaMatch>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_F_US"/>
<rdf:type rdf:resource="http://qudt.org/schema/qudt/QuantityKind"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DeciN"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DYN"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PlanckForce"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MegaLB_F"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloPOND"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/OZ_F"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/POND"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GM_F"/>
<rdfs:comment>Applicable units are those of quantitykind:Force</rdfs:comment>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LB_F"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MegaN"/>
<rdfs:label xml:lang="en">Thrust</rdfs:label>
<rdfs:isDefinedBy rdf:resource="http://qudt.org/2.1/vocab/quantitykind"/>
<j.0:plainTextDescription>Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.</j.0:plainTextDescription>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloGM-M-PER-SEC2"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliN"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KIP_F"/>
<j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PDL"/>
<j.0:hasDimensionVector rdf:resource="http://qudt.org/vocab/dimensionvector/A0E0L1I0M1H0T-2D0"/>
</rdf:Description>
</rdf:RDF>
TURTLE
@prefix owl: <http://www.w3.org/2002/07/owl#> .
@prefix rdf: <http://www.w3.org/1999/02/22-rdf-syntax-ns#> .
@prefix rdfs: <http://www.w3.org/2000/01/rdf-schema#> .
@prefix xsd: <http://www.w3.org/2001/XMLSchema#> .
<http://qudt.org/vocab/quantitykind/Thrust>
rdf:type <http://qudt.org/schema/qudt/QuantityKind> ;
<http://purl.org/dc/terms/description> """Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.
The pushing or pulling force developed by an aircraft engine or a rocket engine.
The force exerted in any direction by a fluid jet or by a powered screw, as, the thrust of an antitorque rotor.
Specifically, in rocketry, $ F\\,= m\\cdot v$ where m is propellant mass flow and v is exhaust velocity relative to the vehicle. Also called momentum thrust."""^^<http://qudt.org/schema/qudt/LatexString> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/DYN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/DeciN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/GM_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KIP_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloGM-M-PER-SEC2> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloGM_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloLB_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloPOND> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/LB_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MegaLB_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MegaN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliN> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/N> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/OZ_F> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PDL> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/POND> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PlanckForce> ;
<http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/TON_F_US> ;
<http://qudt.org/schema/qudt/dbpediaMatch> "http://dbpedia.org/resource/Thrust"^^xsd:anyURI ;
<http://qudt.org/schema/qudt/hasDimensionVector> <http://qudt.org/vocab/dimensionvector/A0E0L1I0M1H0T-2D0> ;
<http://qudt.org/schema/qudt/plainTextDescription> "Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system." ;
rdfs:comment "Applicable units are those of quantitykind:Force" ;
rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
rdfs:label "Thrust"@en ;
<http://www.w3.org/2004/02/skos/core#broader> <http://qudt.org/vocab/quantitykind/Force> ;
.
JSON
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,"qname":"quantitykind:Thrust"
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,"applicable unit":"unit:PDL"
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,"description":"Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.\nThe pushing or pulling force developed by an aircraft engine or a rocket engine.\nThe force exerted in any direction by a fluid jet or by a powered screw, as, the thrust of an antitorque rotor.\nSpecifically, in rocketry, $ F\\,= m\\cdot v$ where m is propellant mass flow and v is exhaust velocity relative to the vehicle. Also called momentum thrust."
,"description (plain text)":"Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system."
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JSON-LD
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"description" : "Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.\nThe pushing or pulling force developed by an aircraft engine or a rocket engine.\nThe force exerted in any direction by a fluid jet or by a powered screw, as, the thrust of an antitorque rotor.\nSpecifically, in rocketry, $ F\\,= m\\cdot v$ where m is propellant mass flow and v is exhaust velocity relative to the vehicle. Also called momentum thrust.",
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"comment" : "Applicable units are those of quantitykind:Force",
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