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A neural-network-based large eddy simulation is performed for flow over a circular cylinder. To predict the subgrid-scale (SGS) stresses, we train two fully connected neural network (FCNN) architectures with and without fusing information from two separate single-frame networks (FU and nFU, respectively), where the input variable is either the strain rate (SR) or the velocity gradient (VG). As the input variables, only the grid-filtered variables are considered for the SGS models of G-SR and G-VG, and both the grid- and test-filtered variables are considered for the SGS models of T-SR and T-VG. The training data are the filtered direct numerical simulation (fDNS) data at $Re_d=3900$ based on the free-stream velocity and cylinder diameter. Using the same grid resolution as that of the training data, the performances of G-SR and G-VG (grid-filtered inputs) and T-SR-FU and T-VG-FU (grid- and test-filtered inputs with fusion) are better than those of the dynamic Smagorinsky model and T-SR-nFU and T-VG-nFU (grid- and test-filtered inputs without fusion). These FCNN-based SGS models are applied to untrained flows having different grid resolutions from that of training data. Although the performances of G-SR and G-VG are degraded, T-SR-FU and T-VG-FU still provide good performances. Finally, T-SR-FU and T-VG-FU trained at $Re_d = 3900$ are applied to higher-Reynolds-number flows ($Re_d = 5000$ and 10 000) and their results are also in good agreements with those of fDNS and previous experiment, indicating that adding the test-filtered variables and fusion increases the prediction capability even for untrained Reynolds number flows.
In this work, we present a pair of tools to improve the fiducial tracking and reconstruction quality of cryo-scanning transmission electron tomography (STET) datasets. We then demonstrate the effectiveness of these two tools on experimental cryo-STET data. The first tool, GoldDigger, improves the tracking of fiducials in cryo-STET by accommodating the changed appearance of highly defocussed fiducial markers. Since defocus effects are much stronger in scanning transmission electron microscopy than in conventional transmission electron microscopy, existing alignment tools do not perform well without manual intervention. The second tool, Checkers, combines image inpainting and unsupervised deep learning for denoising tomograms. Existing tools for denoising cryo-tomography often rely on paired noisy image frames, which are unavailable in cryo-STET datasets, necessitating a new approach. Finally, we make the two software tools freely available for the cryo-STET community.
The Lamb–Chaplygin dipole (Lamb, Hydrodynamics, 2nd edn, 1895, Cambridge University Press; Lamb, Hydrodynamics, 3rd edn, 1906, Cambridge University Press; Chaplygin, Trudy Otd. Fiz. Nauk Imper. Mosk. Obshch. Lyub. Estest., vol. 11, 1903, pp. 11–14) is one of the few closed-form relative equilibrium solutions of the two-dimensional (2-D) Euler equation characterized by a continuous vorticity distribution. We consider the problem of its linear stability with respect to 2-D circulation-preserving perturbations. It is demonstrated that this flow is linearly unstable, although the nature of this instability is subtle and cannot be fully understood without accounting for infinite-dimensional aspects of the problem. To elucidate this, we first derive a convenient form of the linearized Euler equation defined within the vortex core which accounts for the potential flow outside the core while making it possible to track deformations of the vortical region. The linear stability of the flow is then determined by the spectrum of the corresponding operator. Asymptotic analysis of the associated eigenvalue problem shows the existence of approximate eigenfunctions in the form of short-wavelength oscillations localized near the boundary of the vortex and these findings are confirmed by the numerical solution of the eigenvalue problem. However, the time integration of the 2-D Euler system reveals the existence of only one linearly unstable eigenmode and since the corresponding eigenvalue is embedded in the essential spectrum of the operator, this unstable eigenmode is also shown to be a distribution characterized by short-wavelength oscillations rather than a smooth function. These findings are consistent with the general results known about the stability of equilibria in 2-D Euler flows and have been verified by performing computations with different numerical resolutions and arithmetic precisions.
Most simple ailerons produce adverse yaw. However, with proper aileron placement and wing twist, an aileron can produce proverse or neutral yaw, eliminating the need for aileron-rudder mixing, differential aileron deflection or Frise ailerons. The relationship between wing planform, aileron placement and lift distribution is studied here for a special class of optimal lift distributions that minimise induced drag for a variety of design constraints. It is shown that a wing employing the elliptic lift distribution will always produce adverse yaw, independent of aileron design or operating condition. However, for wings employing other optimal lift distributions, the ailerons can be placed to produce proverse or neutral yaw. A numerical lifting-line algorithm is used to explore the impact of aileron design on a wide range of wing planforms and lift distributions. Results can be used in the early stages of design to correctly place ailerons with respect to desired roll-yaw coupling.
In order to clarify and visualize the real state of the structural performances of ships in operation and establish a more optimal, data-driven framework for ship design, construction and operation, an industry-academia joint R&D project on the digital twin for ship structures (DTSS) was conducted in Japan. This paper presents the major achievements of the project. The DTSS aims to grasp the stress responses over the whole ship structure in waves by data assimilation that merges hull monitoring and numerical simulation. Three data assimilation methods, namely, the wave spectrum method, Kalman filter method, and inverse finite element method were used, and their effectiveness was examined through model and full-scale ship measurements. Methods for predicting short-term extreme responses and long-term cumulative fatigue damage were developed for navigation and maintenance support using statistical approaches. In comparison with conventional approaches, response predictions were significantly improved by DTSS using real response data in encountered waves. Utilization scenarios for DTSS in the maritime industry were presented from the viewpoints of navigation support, maintenance support, rule improvement, and product value improvement, together with future research needs for implementation in the maritime industry.
Despite the growing availability of sensing and data in general, we remain unable to fully characterize many in-service engineering systems and structures from a purely data-driven approach. The vast data and resources available to capture human activity are unmatched in our engineered world, and, even in cases where data could be referred to as “big,” they will rarely hold information across operational windows or life spans. This paper pursues the combination of machine learning technology and physics-based reasoning to enhance our ability to make predictive models with limited data. By explicitly linking the physics-based view of stochastic processes with a data-based regression approach, a derivation path for a spectrum of possible Gaussian process models is introduced and used to highlight how and where different levels of expert knowledge of a system is likely best exploited. Each of the models highlighted in the spectrum have been explored in different ways across communities; novel examples in a structural assessment context here demonstrate how these approaches can significantly reduce reliance on expensive data collection. The increased interpretability of the models shown is another important consideration and benefit in this context.
We report a home-built velocity-gradient-tensor-resolved particle image velocimetry (VGTR-PIV) system which spatio-temporally resolves all components of the velocity gradient tensor. This technique is applied to the paradigmatic turbulent Rayleigh–Bénard convection system in a cylindrical cell at three representative positions, i.e. centre, side and bottom regions. The VGTR-PIV system allows us to directly measure, for the first time, the spatio-temporally resolved energy dissipation rate and enstrophy in turbulent thermal convection. In the experiment, the Rayleigh number $Ra$ varied in the range $2 \times 10^8 \leqslant Ra \leqslant 8 \times 10^9$ and the Prandtl number $Pr$ was fixed at $Pr = 4.34$. Compared with the fully resolved energy dissipation rate $\varepsilon$, the pseudo-dissipation provides the best estimate within $3\,\%$, the planar (two-dimensional) surrogate has a larger relative error and the one-dimensional surrogate leads to the largest error. The power-law scalings of the time-averaged energy dissipation rate with the Rayleigh number follow $\langle \varepsilon _c \rangle _t / (\nu ^3 H^{-4}) = 9.86 \times 10^{-6} Ra^{1.54 \pm 0.02}$, $\langle \varepsilon _s \rangle _t / (\nu ^3 H^{-4}) = 9.26 \times 10^{-3} Ra^{1.25 \pm 0.02}$ and $\langle \varepsilon _b \rangle _t / (\nu ^3 H^{-4}) = 2.70 \times 10^{-2} Ra^{1.23 \pm 0.02}$ in the centre, side and bottom regions, respectively where $\nu$ is dynamic viscosity and $H$ is cell height. These scaling relations, along with our earlier measured time-averaged energy dissipation rate at the bottom wall surface $\langle \varepsilon _w \rangle _t / (\nu ^3 H^{-4}) = 9.65 \times 10^{-2} Ra^{1.25 \pm 0.02}$ (J. Fluid Mech., vol. 947, 2022, A15), provide important constraints against which theoretical models may be tested. For the centre and side locations in the convection cell, the probability density functions (p.d.f.s) of the energy dissipation rate and enstrophy both follow a stretched exponential distribution. For the bottom region, the p.d.f.s of dissipation and enstrophy exhibit a stretched exponential distribution outside the viscous boundary layer and an exponential distribution inside the viscous boundary layer. It is also found that extreme events with high dissipation are the most intermittent in the side region, whereas the bottom region is less intermittent than the cell centre.
What are trending Islamic ideas in Southeast Asia; how are they transmitted and who transmits them? These are questions that linger among the minds of policymakers, diplomats and scholars interested in Islam in Southeast Asia. Trending Islam maps and discusses key personalities, groups or institutions that influence Muslims in the region. This book dedicates more space to discuss the role of the Internet in disseminating religious discourses. Internet's role, in particular the use of social media either to advance interpretations of Islamic ideas or to gain influence in the public sphere, is becoming more significant as it allows information to spread faster and wider. While not discounting traditional issues such as extremism and terrorism, matters that continue to affect many people's lives in the region, the book delves into the interaction between violent and non-violent extremism and the liberal and progressive responses to them. Trending Islam covers the transmission of Islam in several countries and some case studies.
The most successful British jet fighter produced was without doubt the sleek and graceful Hawker Hunter. As usual for every new aircraft type it had its share of teething problems, but once these were all adequately solved the U.K. had at that time one of the best jet fighters available. It was built in large numbers and exported to many countries.
Malaysia is a signatory of the Global Methane Pledge, but the implications for national action on methane emissions remain unclear. A review of publicly available literature and data revealed that there is no clear national plan for methane action yet. Since signing the Pledge in 2021, there has been no demonstrable government initiative focusing on joined-up methane action at the national level. Malaysia does not have a methane strategy or policy, and sector-specific regulations focusing on methane emissions are either not present, vague, or publicly inaccessible.
There are indications emissions are falling due to positive corporate action. Effective methane reduction initiatives exist in Malaysia's top two methane-emitting sectors, oil and gas and palm oil, and key players have committed to net zero pathways with methane reductions central to progress to 2030.
Quantifying reductions with confidence remains challenging. Different reporting approaches and incomplete information on assumptions and uncertainties in quantification approaches, make independent analyses of reported emissions challenging.
Improvements in corporate Monitoring, Reporting, and Verification (MRV) in the coming years are expected.
Methane reduction is a 'low-hanging fruit'. Methane is a major initial lever to reduce greenhouse gas emissions up to 2030 in the climate plans of leading Malaysian industry players. Action to improve methane-related processes in the key oil and gas and palm oil sectors thus presents a valuable opportunity for Malaysia to contribute to global climate mitigation within its long-term national interests.
In 1937 The Glen Martin company started with the design of the model I62. This was a design for a twin engine high-wing monoplane flying boat with an inverted gull wing. As power plant one of the most powerful air-cooled radial engines then available was selected: the Wright R-200-6 Cyclone of 1600 hp maximum take-off power.
From 1949 to 2006 the English Electric Canberra has served in the frontline of the Royal Air Force around the world. The Canberra became the UK's first jet bomber, although that was not its only role, undertaking other tasks such as, pilot/navigator training, photographic reconnaissance, target-tag and electronic countermeasures duties to name a few.
The story of the Canberra came to a close for the RAF on the 22nd June 2006 when the last remaining Canberra PR.9s retiring from service life after returning from operational duties. The author had the honour to serve with them in their twilight days of their careers.
When Hungary got involved in World War II, the WM-21 Sólyom (Falcon) was the only Hungarian designed and manufactured plane in service with the Hungarian Royal Airforce. It was in widespread service as reconnaissance plane starting from 1938 onwards. In June of 1941, the machines failed to make an impression, mainly because of accidents and technical issues. The planes were diverted to the training role and were still used as such by May 1945.
The Sólyom story starts in 1927, with the Fokker C.V, of which the Hungarian Royal Airforce had acquired 76, mostly built under license by Manfred Weiss (WM). WM improved the C.V, which resulted in the WM-16, with 18 built in two variants. This WM-16 paved the way for the WM-21, of which 128 examples were built.
One of the lesser-known fighter aircraft of World War II was the Brewster Buffalo, or, using the U.S. Navy designation system, the F2A. By some historians the Buffalo is regarded as an outright failure, but this is a rating this stubby little fighter did not deserve.
This book presents an overview of the development and operational use of the Buffalo with many photos including a number not published before.
Designed in 1933, the elegant looking Fokker C.X was outdated from the start. The type was intended as strategic reconnaissance plane but was not suited for this task. More modern, twin-engine types had claimed this specialized role. Instead, the biplane served well as short range scout and light bomber.
The C.X is a little-known member of the Dutch Fokker stable. Just like the D.XXI this biplane served in the air forces of two little neutral countries on the eve of World War II. Both fought gallantly in a war of David versus Goliath proportions, and the complete operational history of the type spans a total of 25 years. In retrospect, the C.X was the last fighting biplane type built by Fokker and the company's last pre-war military type to survive.
The onset of convection in a horizontal porous medium layer saturated with a nanofluid and heated from below is investigated via linear stability analysis and numerical simulation. The Darcy–Buongiorno model is used to describe the convective transport behaviour of the nanofluid and the settling effect of nanoparticles due to gravity is considered in addition to thermophoresis and Brownian diffusion. The linear stability analysis shows that the gravity settling is a substantial stabilizing mechanism restraining the destabilizing factors such as thermal buoyancy and thermophoresis. The stability threshold is determined by the relative strength of thermophoresis to gravity settling. It is found that the system is destabilized when the thermophoretic mobility prevails. As the nanoparticle size increases, the gravity settling effect is promoted and makes the system more stable. In particular, the onset of instability is dominated by the oscillatory mode once the nanoparticle concentration is in a stably stratified profile across the porous layer. When the Rayleigh–Darcy number $Ra_D$ exceeds the critical value, the spectrum of the growth rates of the unstable modes rises with increasing $Ra_D$ and $Rn$ (i.e. the concentration Rayleigh number), and eventually the unstable modes in the high-wavenumber region exhibit the same instability. The evolution of the convection is further examined by numerical simulation. The results verify the stability characteristics predicted by linear stability analysis. Moreover, the pattern of fingering convection of the nanofluid concentration is observed once the nanofluid concentration is unstably stratified and the density difference across the porous layer is large enough.
After the end of the World War I, the kingdom of Hungary, was – among many other harsh conditions – not allowed to have an armed air force. Aircraft manufacture was completely banned by the Allied as well.
After 1923 the situation improved. Light civilian aircraft were allowed to be built again, but early attempts to build aircraft were not very successful. From March 1927 on, when the strict Allied supervision on Hungary ended, negotiations with foreign aircraft manufacturers were started at once. Secretly, the Dutch company Fokker was already contacted in 1926.
The Dutch aircraft manufacturer Fokker was one of the investigated constructors. A first result was an order for a group of four C.5D reconnaissance planes. The contract was signed on 27 January 1927 and the aircraft were delivered between 20 and 26 June the same year. They were ferried through Austria to Hungary. A next group of four machines was ordered on 28 March 1928. Amongst these, a C.5E was delivered, with a wingspan of 15,3.m, compared to the C.5D’s span of 12,48.m. These aircraft arrived in the spring of 1928.
After testing the C.5D’s would be used as tactical (short range) reconnaissance planes and the C.5E as light bomber. The LÜH (Légügyi Hivatal, the bureau for aeronautical affairs) also decided that the machines were highly suitable for local production. A licence contract was signed in March 1928.
A little while later, on 9 July, the Hungarian company Weiss Manfréd Muvek (WMM) established an aircraft division. This newly formed department would take care of licence production. Rights for aircraft engine production were acquired as well.
Production of one single C.5D and one C.5E started in the second half of 1928. Both were powered by Jupiter VI engines of 520 hp. Performance with this engine was substantially improved. The first machine was completed in December 1928. After trials were completed it was decided that only the C.5D would be built.
During production a number of modifications in the design were applied. Stronger N-struts were used while the undercarriage was replaced by a lighter version of Italian origin. Production was concluded in the fall of 1931. W.M.M. built 49 C.5D’s and a single C.5E.
Solid particles trapped in an acoustic standing wave have been observed to undergo propulsion. This phenomenon has been attributed to the generation of a steady streaming flow, with a reversal in the propulsion direction at a distinct frequency. We explain the mechanism underlying this reversal by considering the canonical problem of a sphere executing oscillatory rotation in an unbounded fluid that undergoes rectilinear oscillation; these two oscillations occur at identical frequency but with an arbitrary phase difference. Two distinct bifurcations in the flow field occur: (1) a stagnation point first forms with increasing frequency, which (2) splits into a saddle node and a vortex centre. Reversal in the propulsion direction is driven by reversal in the flow far from the sphere, which coincides with the second bifurcation. This flow is identified with that of a Stokeslet whose strength is the net force exerted on the particle, which has implications for studying the flow field around particles of non-spherical geometries and for modelling suspensions of particles in acoustic fields.