Laval nozzle

GPTKB entity

Statements (61)
Predicate Object
gptkbp:instanceOf nozzle
gptkbp:appliesTo gas dynamics
gptkbp:createdBy supersonic flow
gptkbp:designedFor accelerating fluid
gptkbp:hasEvents Mach_1_at_the_throat
https://www.w3.org/2000/01/rdf-schema#label Laval nozzle
gptkbp:isAssociatedWith pressure recovery
gptkbp:isAttendedBy computational fluid dynamics
gptkbp:isAvenueFor performance metrics
gptkbp:isCharacterizedBy area ratio
gptkbp:isCriticizedFor space exploration
aerodynamic efficiency
performance optimization
launch vehicle performance
gptkbp:isDesignedFor reduce noise
high-altitude performance
maximize thrust
minimize shock waves
gptkbp:isEvaluatedBy efficiency
environmental impact
thrust-to-weight ratio
computational simulations
gptkbp:isFoundIn spacecraft propulsion systems
gptkbp:isFundedBy high-temperature materials
gptkbp:isIncorporatedIn turbofan engines
gptkbp:isInfluencedBy thermodynamic properties
gptkbp:isIntegratedWith control systems
launch vehicles
gptkbp:isOptimizedFor mass flow rate
gptkbp:isPartOf propulsion systems
engine assembly
nozzle design
engine cycle
engine design process
gptkbp:isRelatedTo aerospace engineering
expansion fans
gptkbp:isSubjectTo flow separation
thermal loads
gptkbp:isTestedFor structural integrity
thermal stability
gptkbp:isTrainedIn wind tunnels
aerodynamic drag
aerodynamic laboratories
gptkbp:isUsedBy control exhaust velocity
gptkbp:isUsedFor specific impulse
turbomachinery
gptkbp:isUsedIn liquid rocket engines
suborbital flights
turbine engines
aircraft propulsion
gptkbp:isUtilizedFor high-speed flight
thrust generation
gptkbp:isUtilizedIn research and development
hypersonic vehicles
satellite propulsion
missile technology
experimental propulsion systems
gptkbp:namedAfter gptkb:Henri_Laval
gptkbp:operatedBy converging and diverging sections
gptkbp:usedIn jet engines
rocket engines