[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Wu et al., 2021 - Google Patents

Visualization and analysis on the thrust vectoring control in three-dimensional dual-throat nozzles

Wu et al., 2021

View PDF
Document ID
1482652710770279157
Author
Wu K
Kim T
Kim H
Publication year
Publication venue
Journal of Visualization

External Links

Snippet

The dual-throat vectoring nozzle is an efficient technique utilizing less high-pressure secondary streams to control mainstream deflections flexibly. In this article, three- dimensional Reynolds-averaged Navier–Stokes simulations were performed using a …
Continue reading at www.researchgate.net (PDF) (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods

Similar Documents

Publication Publication Date Title
Wang et al. Computational study of axisymmetric divergent bypass dual throat nozzle
Aabid et al. Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods
Waithe et al. An experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring
Li et al. Unstart/restart hysteresis characteristics analysis of an over–under TBCC inlet caused by backpressure and splitter
Yagle et al. Demonstration of fluidic throat skewing for thrust vectoring in structurally fixed nozzles
Li et al. Design and investigation on variable Mach number waverider for a wide-speed range
Zhang et al. Control of cowl-shock/boundary-layer interactions by deformable shape-memory alloy bump
Wu et al. Theoretical and numerical analyses of aerodynamic characteristics on shock vector control
Wu et al. Visualization and analysis on the thrust vectoring control in three-dimensional dual-throat nozzles
Wu et al. Study of the streamwise location of a micro vortex generator for a separation-control mechanism in supersonic flow
Wu et al. Sensitivity analysis of counterflow thrust vector control with a three-dimensional rectangular nozzle
Wang et al. Study of starting problem of axisymmetric divergent dual throat nozzle
Wang et al. Design and preliminary analysis of the variable axisymmetric divergent bypass dual throat nozzle
Wu et al. Numerical study of fluidic thrust vector control using dual throat nozzle
Jingwei et al. Numerical investigation on a new concept of shock vector control nozzle
Shi et al. Mechanism of hysteresis and uncontrolled deflection in jet vectoring control based on Coanda effect
Ferlauto et al. Computational investigation of injection effects on shock vector control performance
Jammalamadaka et al. Lattice-Boltzmann very large eddy simulations of fluidic thrust vectoring in a converging/diverging nozzle
Shi Performance estimation for fluidic thrust vectoring nozzle coupled with aero-engine
Wu et al. Assessment of the counter-flow thrust vector control in a three-dimensional rectangular nozzle
Soundararajan et al. Numerical study on strut insertion based thrust vectoring control system
Aabid et al. Numerical analysis of a microjet-based method for active flow control in convergent-divergent nozzles with a sudden expansion duct
Li et al. Numerical study on rod thrust vector control for physical applications
Wang et al. Fourier mode decomposition of unsteady flows in a single injection port fluidic thrust vectoring nozzle
Halwas Side Gust Effects on the Performance of Supersonic Inlet with and without Bleed System using RANS and URANS