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 |