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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
Multi-objective nozzle design optimization for maximum thrust vectoring performance
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
Numerical Simulation on Optimization of Pintle Base Shape in Planar Expansion-Deflection Nozzles
Model-based design of a variable nozzle turbocharger controller
Fast Precision Margin with the First-Order Reliability Method
Optimization of a Mach-6 Quiet Wind-Tunnel Nozzle
Design and Development of a Pneumatic Braking Device for Testing the Gas Turbine Plant
Coupled Fluid–Structure Interaction Analysis of Solid Rocket Motor with Flexible Inhibitors
Two-Zone Model for Predicting the Trajectory of Liquid Jet in Gaseous Crossflow