AI Networking Cookbook: Practical recipes for AI-assisted network automation and development
A Direct Numerical Simulation (DNS) investigates transonic flow over a NACA0012 airfoil coupled with single-DOF structural dynamics. Analysis is performed for angle of attack ({\alpha}) 8{\deg} with varying reduced velocity (U*) from 2 to 8, reduced mass (m*) 5.0, Reynolds number (Re_\infty) of 3 \times 10^6, and Mach...
Experimental data at flight-relevant Reynolds numbers remain scarce for publicly available transport aircraft standard models. This study analyses Reynolds number effects on the CHN-T1 large-aspect-ratio configuration using measurements from the cryogenic European Transonic Wind Tunnel, covering Mach 0.20–0.90 and unit...
This study examines the aerodynamic efficacy of the S809 airfoil at six angles of attack: ?14.23°, ?5.15°, 0°, 5.13°, 9.22°, and 10.21°. It uses steady two-dimensional RANS with two closures: k–? SST (Menter) and k–? Standard. It also checks the results against wind-tunnel data from NREL. We digitized experimental pres...
The aerodynamic performance of conventional (rounded leading-edge) and reversed (sharp leading-edge) airfoils is investigated in the low Reynolds number regime. Computations are performed in the range Re ∈ [1x108, 8x104]. The results show significant differences in the flow structures and the aerodynamic characteristic...
We use direct numerical simulations to study the turbulent transonic flow over a supercritical airfoil, spanning the transition from stable conditions to fully developed buffet at chord-based Reynolds numbers of $3\times10^5$ and $6\times10^5$. The Reynolds number determines the incoming boundary-layer state, thereby a...
Accurately predicting the aerodynamic response of supersonic projectiles under the coupled effects of high-speed spin and non-zero angles of attack (AoA) is critical for trajectory optimisation and submunition dispensing. This study systematically investigates the aerodynamic coupling effects of a 12.7 mm supersonic...
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