NACA airfoil

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instanceOf airfoil
gptkbp:appearsIn aircraft design
wind tunnel testing
gptkbp:characterizedBy thickness
angle of attack
camber
gptkbp:designedBy gptkb:National_Advisory_Committee_for_Aeronautics
gptkbp:developedBy 20th century
gptkbp:hasCountry gptkb:NACA_four-digit_series
gptkb:NACA_five-digit_series
gptkbp:hasRelatedPatent commercial aircraft
drones
military aircraft
gliders
model aircraft
gptkbp:hasType symmetrical airfoil
cambered airfoil
https://www.w3.org/2000/01/rdf-schema#label NACA airfoil
gptkbp:influencedBy gptkb:Newton's_laws_of_motion
Bernoulli's_principle
gptkbp:isBasedOn aerodynamic principles
airfoil theory
gptkbp:isEvaluatedBy computational fluid dynamics
experimental testing
gptkbp:isOptimizedFor performance
efficiency
stability
control
gptkbp:isPartOf aerodynamic design
aerodynamic shapes
aircraft wing design
airfoil family
gptkbp:isReferencedIn aerospace engineering
mechanical engineering
aviation history
aircraft performance analysis
gptkbp:isRelatedTo aerodynamic efficiency
airfoil design
lift-to-drag ratio
stall characteristics
boundary layer
gptkbp:isStudiedIn fluid dynamics
gptkbp:isTrainedIn flight tests
simulation software
wind tunnels
gptkbp:isUsedBy students
researchers
aerospace engineers
aircraft designers
gptkbp:provides lift
drag characteristics
gptkbp:usedIn aerodynamics