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Flow asymmetry in a y-shaped diverterless supersonic inlet: A novel finding
, Article AIAA Journal ; Volume 58, Issue 6 , 2020 , Pages 2609-2620 ; Soltani, M. R ; Sharif University of Technology
American Institute of Aeronautics and Astronautics Inc
2020
Abstract
Extensive wind-tunnel tests were performed on a Y-shaped diverterless supersonic inlet (DSI). All tests were conducted at a free stream Mach number of M∞ 1.65, the design Mach number for this inlet, and at both zero degrees angle of attack (AOA) and angle of sideslip (AOS). The experiments were performed at various inlet operating conditions comprising supercritical, critical, and subcritical conditions that covered almost all ranges of the engine operating for this DSI. The results showed that the DSI had relatively acceptable performance characteristics when operating at its design condition. A symmetric supersonic flow pattern was observed at both supercritical and critical operating...
Symmetric and asymmetric performance investigation of a diverterless supersonic inlet
, Article AIAA Journal ; Volume 60, Issue 5 , 2022 , Pages 2850-2859 ; 00011452 (ISSN) ; Soltani, M. R ; Sharif University of Technology
AIAA International
2022
Abstract
A series of wind-tunnel tests were conducted on a Y-shaped diverterless supersonic inlet (DSI) in order to investigate its performance at various operating conditions. The present DSI was designed for a freestream Mach number of M∞ 1.65. The experiments were performed at supercritical, critical, and subcritical operating conditions and at 0 deg angle of attack and angle of side slip. The results showed that the present DSI had an acceptable performance at its design condition. A symmetric supersonic flow pattern was observed at both supercritical and critical operating conditions. At low subcritical operating conditions, the supersonic flow pattern remained symmetric too. However, at high...
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet
, Article Journal of Aircraft ; Volume 60, Issue 4 , 2023 , Pages 1007-1016 ; 00218669 (ISSN) ; Soltani, M. R ; Sharif University of Technology
AIAA International
2023
Abstract
Three-dimensional (3-D) numerical simulations of a Y-shaped body-integrated diverterless supersonic inlet (DSI) have been investigated. A diverterless supersonic inlet is an external supersonic flow compression that uses a 3-D geometry of a bump for both supersonic flow compression and boundary-layer diversion. The simulations are performed in the presence of a typical body comprising an elliptical nose in order to model a more realistic approaching flow to the inlet entrance. All simulations were performed at a freestream Mach number of M∞ 1.65, the design Mach number, and at a 0 deg angle of attack (AOA) and 0 deg angle of sideslip (AOS). The Navier–Stokes relations along with k-ω shear...
Multiphysics modeling of an MSMA-based clamped-clamped inertial energy harvester
, Article Smart Materials and Structures ; Volume 28, Issue 3 , 2019 ; 09641726 (ISSN) ; Zakerzadeh, M. R ; Sharif University of Technology
Institute of Physics Publishing
2019
Abstract
In this paper, an alternative way of harvesting energy from ambient vibration is investigated through proposing a novel inertial energy harvester using magnetic shape memory alloys (MSMAs). To this end, a clamped-clamped beam is coupled with MSMA units which are attached to its roots. A shock load is applied to a proof mass in the middle of the beam. The beam vibration causes longitudinal strain in the MSMAs and as a result the magnetic flux alters in the coils wounding around the MSMA units and produce an AC voltage. To have a reversible strain in MSMAs, a bias magnetic field is applied in transverse direction of the MSMA units. The large scale vibration of Euler-Bernoulli beam is modeled...
Observer-based adaptive neural network controller for uncertain nonlinear systems with unknown control directions subject to input time delay and saturation
, Article Information Sciences ; Volume 418-419 , 2017 , Pages 717-737 ; 00200255 (ISSN) ; Shahrokhi, M ; Askari, M. R ; Sharif University of Technology
2017
Abstract
This paper addresses the design of an observer based adaptive neural controller for a class of strict-feedback nonlinear uncertain systems subject to input delay, saturation and unknown direction. The input delay has been handled using an integral compensator term in the controller design. A neural network observer has been developed to estimate the unmeasured states. In the observer design, the Lipschitz condition has been relaxed. To solve the problem of unknown control directions, the Nussbaum gain function has been applied in the backstepping controller design. “The explosion of complexity” occurred in the traditional backstepping technique has been avoided utilizing the dynamic surface...
Numerical simulation of mixed compression intake Buzz
, Article ASME 2017 International Mechanical Engineering Congress and Exposition, IMECE 2017, 3 November 2017 through 9 November 2017 ; Volume 1 , 2017 ; 9780791858349 (ISBN) ; Abedi, M ; Askari, R ; ASME ; Sharif University of Technology
American Society of Mechanical Engineers (ASME)
2017
Abstract
Numerical analysis has been conducted to simulate and capture Buzz phenomenon in a supersonic mixed compression air intake. Buzz is an unsteady self-sustained phenomenon occurred in supersonic intakes, especially when operating its subcritical condition, during which the system of compression and shock waves oscillate and move upstream and downstream along the intake. An axisymmetric and unsteady numerical simulation was used to solve Navier-Stokes equations in combination with URANS SST k-ω turbulence model The simulations were performed at M=2.0 and at a specific subcritical point of the intake operation where buzz was detected experimentally. Results are compared with experimental...
A novel inertial energy harvester using magnetic shape memory alloy
, Article Smart Materials and Structures ; Volume 25, Issue 10 , 2016 ; 09641726 (ISSN) ; Sayyaadi, H ; Zakerzadeh, M. R ; Sharif University of Technology
Institute of Physics Publishing
2016
Abstract
This paper studies the output voltage from a novel inertial energy harvester using magnetic shape memory alloys (MSMAs). The MSMA elements are attached to the root of a cantilever beam by means of two steps. In order to get electrical voltage, two coils are wound around the MSMAs and a shock load is applied to a tip mass at the end of the beam to have vibration in it. The beam vibration causes strain in the MSMAs along their longitudinal directions and as a result the magnetic flux alters in the coils. The change of magnetic flux in the surrounding coil produces an AC voltage. In order to predict the output voltage, the nonlinear governing equations of beam motion based on Euler-Bernoulli...
Size influence of specimens and maximum aggregate on dam concrete: compressive strength
, Article Journal of Materials in Civil Engineering ; Volume 21, Issue 8 , 2009 , Pages 349-355 ; 08991561 (ISSN) ; Mohamadi Shooreh, M. R ; Askari, S. M ; Sharif University of Technology
2009
Abstract
The compressive strength of mass concrete in dams is obtained from laboratory experiments of various cylindrical specimens with diameters of 150, 250, and 300 mm, and heights of 300, 500, and 450 mm, respectively. These specimens with 37.5, 75, and 150 mm maximum size of aggregate were investigated. The 7- and 90-day compressive strength of concrete was found to be between 20 and 58 MPa depending on the size of the specimens. The results reveal the existence of a significant size effect. Based on test results, relationships between the strength of mass concrete specimens and their size and shape are developed. Finally, results and a discussion are presented regarding compressive strength...
Effects of wing geometry on wing-body-tail interference in subsonic flow
, Article Scientia Iranica ; Volume 18, Issue 3 B , 2011 , Pages 407-415 ; 10263098 (ISSN) ; Soltani, M. R ; Askari, F ; Pajuhande, H. R ; Sharif University of Technology
2011
Abstract
Extensive wind tunnel tests were performed on several wing- body-tail combinations in subsonic flow to study the effects of wing geometric parameters on the flow field over the tail. For each configuration, tail surface pressure distribution, as well as the velocity contour at a plane perpendicular to the flow direction behind the wing was measured. The results show a strong effect of wing to tail span ratio, as well as wing aspect ratio, on the flowfield downstream of the wing. For low sweep wings, as those considered here, wing and body interference effects on the tail are associated with the wing tip vortex and nose-body vortex
Detection of thermal infrared (TIR) anomalies related to the M s=5.1 earthquake on Oct. 14, 2004 near Ravar (SE Iran)
, Article Journal of the Earth and Space Physics ; Volume 35, Issue 4 , 2010 ; 03781046 (ISSN) ; Hafezi, N ; Rahimi Tabar, M. R ; Ansari, A. R ; Sharif University of Technology
2010
Abstract
Over the last two decades there have been numerous reports from different seismically active regions of the world that thermal infrared (TIR) anomalies can be identified around the epicentral areas before major earthquakes [e.g. (Tronin et al., 2002)]. The TIR anomalies reportedly appear as early as 14 to 7 days before the seismic events and affect areas as large as 1000s to 100,000s km2 in size. Our case study for detection of TIRs using NOAA-AVHRR data(Band 4) is an Ms = 5.1 earthquake that occurred on 14th October 2004 near Ravar in Kerman province located in Loot and Tabas deserts, southeast-central Iran. The area is part of the Golbaf-Sirj seismogenic zone. It includes major faults...
Geometrical scaling effects on supersonic inlet performance
, Article ASME 2017 International Mechanical Engineering Congress and Exposition, IMECE 2017, 3 November 2017 through 9 November 2017 ; Volume 1 , 2017 ; 9780791858349 (ISBN) ; Soltani, M. R ; Khajeh Fard, A ; ASME ; Sharif University of Technology
American Society of Mechanical Engineers (ASME)
2017
Abstract
The effects of geometrical scaling on a supersonic external compression axisymmetric inlet are investigated. Various lower and higher geometrical scales of supersonic inlet are considered as the case studies. The inlet flow is simulated numerically using RANS solver along with the SST k-w turbulence model. The numerical results are in an acceptable agreement with the NACA experimental data at free stream Mach number of 1.79 and at zero angle of attack. The results show that the static pressure distribution of the inlet flow experiences some differences for various scales especially at the regions of the flow entrance and throat area. The mean flow Mach number and the mass flow rate at the...
Synthesis of cellulose acetate/chitosan/SWCNT/Fe3O4/TiO2 composite nanofibers for the removal of Cr(VI), As(V), Methylene blue and Congo red from aqueous solutions
, Article International Journal of Biological Macromolecules ; Volume 140 , 2019 , Pages 1296-1304 ; 01418130 (ISSN) ; Koushkbaghi, S ; Pishnamazi, M ; Askari, A ; Khosravi, R ; Irani, M ; Sharif University of Technology
Elsevier B.V
2019
Abstract
The potential of electrospun cellulose acetate/chitosan/single walled carbon nanotubes/ferrite/titanium dioxide (CA/chitosan/SWCNT/Fe3O4/TiO2) nanofibers was investigated for the removal of Cr(VI), As(V), Methylene blue and Congo red from aqueous solutions via the adsorption and photocatalytic reduction processes. The properties of synthesized SWCNT/Fe3O4/TiO2 and fibers were characterized using TEM, SEM, FTIR, XRD, TGA and BET analysis. In adsorption process, the influence of adsorbent type including SWCNT to Fe3O4 ratio, TiO2 to SWCNT/Fe3O4 ratio and SWCNT/Fe3O4/TiO2 concentration as well as the adsorption parameters including pH, contact time, and initial concentration of adsorbates on...
Non-linear assessment of tunable vibrating ring micro-gyroscopes design
, Article Mechanics Based Design of Structures and Machines ; 2023 ; 15397734 (ISSN) ; Mokhtari Amir Majdi, M. A ; Askari, A. R ; Sharif University of Technology
Taylor and Francis Ltd
2023
Abstract
This paper introduces a tunable design for an electrically actuated vibrating ring micro-gyroscope. This mechanism contains eight piezoelectric micro-beams attached to the vibrating ring in each drive and sense directions. Employing a full geometric non-linear model for the vibrating ring and accounting for the micro-beam’s mid-plane stretching; the mathematical model associated with the present system is obtained. Afterward, utilizing the Hamilton principle together with the Ritz method, the reduced equations of motion are derived. The present results are validated by those available in the literature for simpler systems. A three-dimensional (3D) finite element (FE) simulation was carried...
Modeling and simulation of flow and uranium isotopes separation in gas centrifuges using implicit coupled density-based solver in OpenFOAM
, Article European Journal of Computational Mechanics ; Volume 29, Issue 1 , 2020 , Pages 1-26 ; Salehi, A. A ; Keshtkar, A. R ; Shadman, M. M ; Askari, M. H ; Sharif University of Technology
River Publishers
2020
Abstract
The performance of a gas centrifuge that is used for isotopes separation is dependent on the gas flow inside it. In this study, for modeling the UF6 gas flow, an Implicit Coupled Density-Based (ICDB) solver, was developed in OpenFOAM. To validate the ICDB solver, the gas flow within the rotor in total reflux state was compared with the analytical solution obtained by Onsager model and the numerical solution obtained by the Fluent software. The results showed that the ICDB solver had acceptable accuracy and validity. Also the computational efficiency of Roe, AUSM (Advection Upstream Splitting Method) and AUSM+ up schemes were compared. The results showed AUSM+ up scheme is efficient. Then,...
Adjoint-based design optimization of s-shaped intake geometry
, Article ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE), 3 November 2017 through 9 November 2017 ; Volume 1 , 2017 ; 9780791858349 (ISBN) ; Shoureshi, P ; Soltani, M. R ; Khajeh Fard, A ; ASME ; Sharif University of Technology
2017
Abstract
The S-shaped air intakes are very common shapes due to their ease in the engine-body integration or Radar Cross Section, RCS, specifications especially for fighter aircrafts. The numerical shape optimization of an S-shaped air intake using adjoint method is conducted. The flow of a specified air intake that uses S-duct M2129 is simulated using three dimensional (3D) numerical solution of Reynolds-Averaged Navier-Stokes equation along with k-ω SST turbulence model. The main purpose of this optimization scheme is to maximize the total pressure recovery (TPR). Further, the scheme is developed in such a way that would be applicable in industry thru satisfying specified constraint requirements....
Laser induced surface processing with gold nanoparticle arrays embedded in a transparent matrix
, Article Nano ; Volume 8, Issue 1 , January , 2013 ; 17932920 (ISSN) ; Bahrampour, A. R ; Sharif University of Technology
2013
Abstract
Gold nanoparticles are widely used as high efficient photon-thermal energy converters in a broad range of applications. This paper presents a theoretical investigation on using the optothermal properties of gold nanoparticle arrays to generate nanoscale molten and rubbery regions on the surface of an amorphous polymeric film. Nanoparticles are assumed to be embedded in a transparent silica layer and illuminated with a 7.5 ns pulsed laser at 532 nm. Simulation results are presented for systems with single gold nanoparticles, dimers and chains. Both electromagnetic and thermal interaction between nanoparticles are found to be important factors in determining the result of surface processing....
A novel approach for energy and water conservation in wet cooling towers by using MWNTs and nanoporous graphene nanofluids
, Article Energy Conversion and Management ; Volume 109 , 2016 , Pages 10-18 ; 01968904 (ISSN) ; Lotfi, R ; Seif Kordi, A ; Rashidi, A. M ; Koolivand, H ; Sharif University of Technology
Elsevier Ltd
2016
Abstract
This study deals with an experimental investigation on the thermal performance of a mechanical wet cooling tower with counter flow arrangement by using multi-walled carbon nanotubes (MWNTs) and nanoporous graphene nanofluids. Stable nanofluids were prepared through two-step procedure by using water with properties taken from a working cooling tower in the South of Iran. Zeta potential revealed suitable stability of MWNTs and nanoporous graphene nanofluids. Thermal and rheological properties of the nanofluids were investigated. It was found that thermal conductivity increases by 20% and 16% at 45°C for MWNTs and nanoporous graphene nanofluids, respectively. The increase in density and...
A new colloidal technique for the synthesis of lead sulfide nanoparticles
, Article Scientia Iranica ; Volume 10, Issue 3 , 2003 , Pages 357-360 ; 10263098 (ISSN) ; Ghamsari, M. S ; Sharif University of Technology
Sharif University of Technology
2003
Abstract
In this paper, the use of colloid chemistry in the synthesis of 5 A° lead sulfide semiconductor nanoparticles has been described. Here, hydrogen sulfide gas dissolved in water is used for the chemical reaction, instead of purging the H2S gas into the solution, which has an influence on particle size. In this technique, the growth of particles was controlled by the addition of EDTA. A fast evolution of the optical absorption spectrum demonstrated the following synthesis. Soon after synthesis reaction, the sample exhibits a structural absorption spectrum with one well-defined peak in a 240 nm wavelength. The absorption spectrum shows a featureless structure, with no tail near the absorption...
Observer-based adaptive fuzzy controller for nonlinear systems with unknown control directions and input saturation
, Article Fuzzy Sets and Systems ; May , 2016 ; 01650114 (ISSN) ; Shahrokhi, M ; Khajeh Talkhoncheh, M ; Sharif University of Technology
Elsevier
2016
Abstract
This paper addresses design of an observer-based adaptive fuzzy controller for a class of single-input-single-output (SISO) nonlinear systems with unknown dynamics subject to input nonlinearity and unknown direction. The proposed controller is singularity free. A high-gain observer is designed to estimate the unmeasured states, and the Lipschitz condition for proving boundedness of the estimated states is relaxed. The Nussbaum function is used to handle the unknown virtual control directions and the backstepping technique has been applied for controller design. It is proved that all closed loop signals are semi-globally uniformly ultimately bounded (SGUUB) and the output tracking error...
Observer-based adaptive fuzzy controller for nonlinear systems with unknown control directions and input saturation
, Article Fuzzy Sets and Systems ; Volume 314 , 2017 , Pages 24-45 ; 01650114 (ISSN) ; Shahrokhi, M ; Khajeh Talkhoncheh, M ; Sharif University of Technology
Elsevier B.V
2017
Abstract
This paper addresses design of an observer-based adaptive fuzzy controller for a class of single-input–single-output (SISO) nonlinear systems with unknown dynamics subject to input nonlinearity and unknown direction. The proposed controller is singularity free. A high-gain observer is designed to estimate the unmeasured states, and the Lipschitz condition for proving boundedness of the estimated states is relaxed. The Nussbaum function is used to handle the unknown virtual control directions and the backstepping technique has been applied for controller design. It is proved that all closed loop signals are semi-globally uniformly ultimately bounded (SGUUB) and the output tracking error...