Results 1 to 10 of about 113 (105)

Blowdown wind tunnel control using an adaptive fuzzy PI controller [PDF]

open access: yesINCAS Bulletin, 2013
The paper presents an approach towards the control of a supersonic blowdown wind tunnel plant (as evidenced by experimental data collected from “INCAS Supersonic Blowdown Wind Tunnel”) using a PI type controller.
Corneliu Andrei NAE
doaj   +2 more sources

Dynamic responses and vibration control of the transmission tower-line system: a state-of-the-art review. [PDF]

open access: yesScientificWorldJournal, 2014
This paper presented an overview on the dynamic analysis and control of the transmission tower‐line system in the past forty years. The challenges and future developing trends in the dynamic analysis and mitigation of the transmission tower‐line system under dynamic excitations are also put forward.
Chen B, Guo WH, Li PY, Xie WP.
europepmc   +2 more sources

Inviscid and viscous interactions in subsonic corner flows. [PDF]

open access: yesScientificWorldJournal, 2013
A flap can be used as a high‐lift device, in which a downward deflection results in a gain in lift at a given geometric angle of attack. To characterize the aerodynamic performance of a deflected surface in compressible flows, the present study examines a naturally developed turbulent boundary layer past the convex and concave corners.
Chung KM, Chang PH, Chang KC.
europepmc   +2 more sources

Intelligent Controller Design for a Blowdown Supersonic Wind Tunnel

open access: yesInternational Journal of Control and Automation, 2014
In this paper, first, the nonlinear mathematical model of special Blowdown Supersonic Wind Tunnel (BSWT) consisting of a set of ordinary differential and algebraic equations is developed in Matlab/Simulink software environment. At the second step, an Artificial Neural Network (ANN) is used for finding the optimum membership functions of the Fuzzy Logic
A. Nazarian Shahrbabaki   +3 more
openaire   +2 more sources

Selection criteria of optimal conditions for supersonic tests in a blowdown wind tunnel [PDF]

open access: yesScientific Technical Review, 2016
A natural desire of a wind tunnel test engineer is to plan and perform a test that will resemble the actual flight conditions as closely as possible. Geometric similarity and identical flight and wind tunnel Mach numbers are the primary requirements and ...
Damljanović Dijana, Vuković Đorđe
doaj   +3 more sources

OPTIMIZED CONTROLLER DESIGN FOR A BLOWDOWN SUPERSONIC WIND TUNNEL BY USING GENETIC ALGORITHM [PDF]

open access: yesمجله مدل سازی در مهندسی, 2017
Blowdown Supersonic Wind Tunnels (SWTs) are generally operated with a constant stagnation pressure in the settling chamber, with control usually provided by one or more pressure regulators or control valves. In this paper, first, a Simulink block diagram
Mehradad Bazazzadeh   +3 more
doaj   +2 more sources

Wind tunnel verification of base-bleed effects on aerodynamic characteristics of an axi-symmetric projectile [PDF]

open access: yesScientific Technical Review, 2021
Experimental verification of base-bleed effects on aerodynamic characteristics for the supersonic flight stages was requested during the development of an axi-symmetric projectile.
Damljanović Dijana   +3 more
doaj   +1 more source

Mode Switching in a Compressible Rectangular Cavity Flow

open access: yesAerospace, 2023
This study determines the mean and fluctuating pressures for flow through a rectangular shallow cavity (ratio between the length and the depth = 2.43, 4.43, and 6.14; ratio between the length and the width = 0.5, 1.0, and 2.0) at a Mach number of 0.64 in
Yi-Xuan Huang, Kung-Ming Chung
doaj   +1 more source

INCAS TRISONIC WIND TUNNEL [PDF]

open access: yesINCAS Bulletin, 2009
The 1.2 m x 1.2 m Trisonic Blowdown Wind Tunnel is the largest of the experimental facilities at the National Institute for Aerospace Research - I.N.C.A.S. "Elie Carafoli", Bucharest, Romania.
Florin MUNTEANU
doaj   +1 more source

Study on the Effect of Oxidative Jet and Vortex Structure in Fluidic Throat Combined with Thrust Vector Control

open access: yesInternational Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023
To examine the impact of oxidative jets on the thrust vector angle, secondary combustion efficiency, and combustion chamber pressure, inert gas (nitrogen) and pure oxygen are injected into the primary flow, which includes combustible components, at various locations in the divergence section and throat using different injection techniques.
Dongfeng Yan   +5 more
wiley   +1 more source

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