Wavelet-based Adaptive Techniques Applied to Turbulent Hypersonic Scramjet Intake Flows [PDF]
, 2013 The simulation of hypersonic flows is computationally demanding due to large gradients of the flow variables caused by strong shock waves and thick boundary or shear layers. The resolution of those gradients imposes the use of extremely small cells in the respective regions.
arxiv +1 more source
Crystalline Assemblies of DNA Nanostructures and Their Functional Properties
Angewandte Chemie, Volume 137, Issue 3, January 15, 2025.This review summarizes recent advancements in DNA tile and DNA origami‐based 2D and 3D crystal lattice assemblies. It covers innovations in monomer design, guest molecule incorporation, and inorganic coating techniques. Key focus areas include assembly strategies, functional properties, structural challenges, and insights for future applications in ...
Xueqiao Li +5 more
wiley +1 more source
Special issue on the fluid mechanics of hypersonic flight
Theoretical and Computational Fluid Dynamics, 2022 V. Theofilis, S. Pirozzoli, P. Martin
semanticscholar +1 more source
Review of control and guidance technology on hypersonic vehicle
Chinese Journal of Aeronautics, 2021 Yibo Ding +3 more
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Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies [PDF]
, 1957 LESTER LEES, TOSHI KUBOTA
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EFFECTS OF COOLING ON TRANSITION IN THE BOUNDARY LAYER ON A HEMISPHERE IN SIMULATED HYPERSONIC FLOW [PDF]
, 1961 Roger A. Dunlap, Arnold M. Kuethe
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A Microwave Method of determining the Displacement and Velocity of a Piston in a Hypersonic Gun Tunnel [PDF]
, 1959 L. Pennelegion
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IEEE Access, 2019 Due to the high maneuverability of a hypersonic vehicle, the measurements for tightly coupled INS/GNSS (inertial navigation system/global navigation satellite system) integration system inevitably involve errors.
Gaoge Hu +4 more
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Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic Speeds [PDF]
, 1953 Ting-Yi Li, H. T. Nagamatsu
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Analysis of thermochemical non-equilibrium hypersonic flow over a waverider with uncertainty quantification [PDF]
arXivThe objective of this work is to assess the impact of parameter uncertainty on hypersonic aerothermal surface heating predictions in Reynolds-Averaged Navier-Stokes (RANS) simulations using non-intrusive uncertainty quantification (UQ) techniques. RANS-based models are considered indispensable tools in computational fluid dynamics (CFD) analysis for ...
arxiv