Calculate the ignition height of the vertical landing phase online for the reusable rocket
For the vertical landing phase of the reusable rocket, in order to improve the landing accuracy with consideration of multiple
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Experimental study of the vortex flow and aerodynamic characteristics of a reverse delta wing
Impact of biofuel blends on the emissions of modern vehicles
Effect of geometric parameters on the spray cone angle in the pressure swirl injector
An optimal design model for the wall thickness of the propellant tank
Mechanism investigation of enhancing the stability of an axial flow rotor by blade angle slots
Simulation model for analysis and evaluation of selected measures of the helicopter’s readiness
The characterisation of a gust generator for aerodynamic testing
Effect of different triple swirlers on the performance of a triple swirler combustor
The importance of controlling the upstream body wake in tandem cylinders system for noise reduction
Investigation of a new flux scheme for the numerical simulation of the supersonic intake flow
Estimation models for the preliminary design of electromechanical actuators