ISQ
12 / 115
11-4.12

lift coefficient

URNurn:iso:std:iso:80000:-11:ed-2:en:item:11-4.12
Download RDF.jsonld.ttl
https://metanorma.github.io/isq-smart/quantities/part-11/t11-4.12
urn:iso:std:iso:80000:-11:ed-2:en:item:11-4.12
ISQ Identifiers
ISO
urn:iso:std:iso:80000:-11:ed-2:en:item:11-4.12
IEC
urn:iec:std:iec:80000-11:2019:::item:11-4.12
Designations
ENlift coefficient
FRcoefficient de portance
Symbol
c l
c A
Notation systems
Rendered
c l
Rendered
c A
AsciiMath
c_"l"
AsciiMath
c_"A"
LaTeX
c_{\text{l}}
LaTeX
c_{\text{A}}

Definition

EN

quotient of the lift force available from a wing at a given angle and the inertial force for a wing shaped body moving in a fluid, expressed by

c l = 2 F l ρ v 2 S = F l q S ; where

F l :: is lift force (ISO 80000-4: Mechanics) on the wing,

ρ :: is mass density (ISO 80000-4: Mechanics) of the fluid,

v :: is speed (ISO 80000-3: Space and time) of the body,

S = A cos α :: is effective area (ISO 80000-3: Space and time) when α is the angle of attack and A is area of the wing, and

q = ρ v 2 / 2 :: is dynamic pressure.

FR

quotient de la force de sustentation développée par une aile à un angle d'incidence donné par la force d'inertie pour un corps en forme d'aile se déplaçant dans un fluide, exprimé par:

c l = 2 F l ρ v 2 S = F l q S ; où

F l :: est la force (ISO 80000-4: Mechanics) de sustentation s'exerçant sur l'aile;

ρ :: est la masse volumique (ISO 80000-4: Mechanics) du fluide;

v :: est la vitesse (ISO 80000-3: Space and time) du corps;

S = A cos α :: est l'aire effective (ISO 80000-3: Space and time) lorsque α est l'angle d'incidence et A est l'aire de l'aile; et

q = ρ v 2 / 2 :: est la pression dynamique

0

Notes

EN

The lift coefficient is dependant on the shape of the wing.

FR

Le coefficient de portance dépend de la forme de l'aile.

Concept HierarchyPendrill (2024)
1dimensionless quantitiesLevel 0 · Kind

Ontology

Class Hierarchy

A physical quantity as defined in ISO/IEC 80000, with associated symbols, definitions, and units of measurement.

Instance IRI

isq:t11-4.12
PropertyValue
rdf:type
dcterms:identifier
11-4.12
skosxl:prefLabel
"lift coefficient"@en
skosxl:altLabel
"c_"l""@en"c_"A""@en
skos:definition
quotient of the lift force available from a wing at a given angle and the inertial force for a wing shaped body moving i…
skos:note
The lift coefficient is dependant on the shape of the wing.
isq:hasDimension
smart:hasBindingnessType
dcterms:isPartOf