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Design
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keywords:(Nozzle Design)
Direct calculation of the average local Mach number in converging–diverging nozzles
Inverse design method on scramjet nozzles based on maximum thrust theory
Performance prediction and optimization for liquid rocket engine nozzle
Calibration strategy of diesel-fuel spray atomization models using a design of experiment method
Calibration strategy of diesel-fuel spray atomization models using a design of experiment method
Design and cold flow test of a scramjet nozzle with nonuniform inflow
Inviscid Nozzle for Aerospike Rocket Engine Application
Optimization design of energy deposition on single expansion ramp nozzle
Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane
Design and Analyses of High Aspect Ratio Nozzles for Distributed Propulsion Acoustic Measurements
Design and Analyses of High Aspect Ratio Nozzles for Distributed Propulsion Acoustic Measurements
Multi-objective nozzle design optimization for maximum thrust vectoring performance
Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane
Design and optimization of three-dimensional supersonic asymmetric truncated nozzle
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing