Aerospace Science and Technology
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Interaction of the wakes of two flapping wings on control forces and moment
Aerospace Science and Technology - Tập 115 - Trang 106794 - 2021
Modeling and switching adaptive control for nonlinear morphing aircraft considering actuator dynamics
Aerospace Science and Technology - Tập 122 - Trang 107349 - 2022
Geometry scaling technique and application to aerodynamic redesign of multi-stage transonic axial-flow compressors
Aerospace Science and Technology - Tập 121 - Trang 107303 - 2022
Geometry scaling technique, as one of the essential steps in aerodynamic redesign of multi-stage compressor, directly determines whether the new scaled geometry meets the required performance or not. It is also one of the effective measures in unsteady flow simulation of multi-stage compressor to reduce greatly the computational cost by scaling the computational domain from full-annulus passages t...... hiện toàn bộ
#Multi-stage transonic compressor #Aerodynamic redesign #Geometry scaling technique #Geometry dissimilarity #Aerodynamic similarity
Lean blowoff behavior of cavity-stabilized flames in a supersonic combustor
Aerospace Science and Technology - Tập 109 - Trang 106427 - 2021
Investigation on the effect of the expansion angle in the strut-based supersonic combustor
Aerospace Science and Technology - Tập 133 - Trang 108095 - 2023
Anti-tangle control of tethered space robots using linear motion of tether offset
Aerospace Science and Technology - Tập 89 - Trang 163-174 - 2019
Experimental study on spray characteristics of fan nozzle for integrated afterburner in lateral airflow
Aerospace Science and Technology - Tập 130 - Trang 107937 - 2022
Non-modal stability analysis of low-Re separated flow around a NACA 4415 airfoil in ground effect
Aerospace Science and Technology - Tập 92 - Trang 269-279 - 2019
Interaction of microwave and laser discharge resulting “heat spots” with supersonic combined cylinder bodies
Aerospace Science and Technology - Tập 43 - Trang 343-349 - 2015
Investigations of a novel boundary condition approach for the accurate prediction of hypersonic oblique shocks in mesh-free Lagrangian simulations
Aerospace Science and Technology - Tập 107 - Trang 106322 - 2020
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