NACA five-digit series

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instanceOf airfoil series
gptkbp:appliesTo airfoil design
gptkbp:basedOn theoretical analysis
experimental data
gptkbp:characterizedBy thickness
maximum camber
position of maximum camber
gptkbp:developedBy gptkb:National_Advisory_Committee_for_Aeronautics
gptkbp:firstIntroduced 1930s
https://www.w3.org/2000/01/rdf-schema#label NACA five-digit series
gptkbp:includes NACA 0012
NACA 2412
NACA 4412
NACA 23012
NACA 64012
gptkbp:isAttendedBy computational fluid dynamics
gptkbp:isDocumentedIn aeronautical research papers
gptkbp:isEvaluatedBy wind tunnel testing
gptkbp:isInfluencedBy fluid dynamics
gptkbp:isPartOf gptkb:NACA_four-digit_series
aerodynamic design
aerodynamic simulations
aerodynamic modeling
aerodynamic research
aircraft performance metrics
aerodynamic optimization
airfoil performance analysis
aircraft performance evaluation
airfoil classification
aircraft design process
aerodynamic characteristics evaluation
aerodynamic efficiency studies
airfoil design methodologies
airfoil optimization techniques
airfoil performance prediction
airfoil selection process
airfoil testing
NACA_six-digit_series
gptkbp:isReferencedIn aerodynamics textbooks
gptkbp:isRelatedTo gptkb:NACA_airfoils
gptkbp:isStudiedIn aeronautical engineering courses
gptkbp:isUsedIn aviation industry
gptkbp:isUtilizedFor universities
research institutions
aerospace engineers
aircraft designers
gptkbp:provides performance characteristics
gptkbp:replacedBy gptkb:NACA_four-digit_series
gptkbp:usedFor aircraft wings
propeller blades
gptkbp:usedIn aerodynamics