Results 21 to 30 of about 81,958 (286)

Aerodynamic characteristics of hypersonic airfoils based on jet flow control technology

open access: yesAIP Advances, 2021
Hypersonic aircraft represent an important area of aerospace development. Raising the aircraft lift-to-drag ratio, improving the efficiency of attitude control, and optimizing aerodynamic performance are important goals.
Jiachen Zhu   +3 more
doaj   +1 more source

Eilmer: an Open-Source Multi-Physics Hypersonic Flow Solver [PDF]

open access: yesComput. Phys. Commun. 282 (2023) Article 108551, 2022
This paper introduces Eilmer, a general-purpose open-source compressible flow solver developed at the University of Queensland, designed to support research calculations in hypersonics and high-speed aerothermodynamics. Eilmer has a broad userbase in several university research groups and a wide range of capabilities, which are documented on the ...
arxiv   +1 more source

COUNTERING HYPERSONIC THREAT

open access: yesBulletin of "Carol I" National Defense University, 2022
Hypersonic missiles represent the new class of threats, capable declaratively and in a way that has not been proven in a theater of operations, to annihilate air and anti-missile defences that exist at this time.
Cătălin CHIRIAC
doaj   +1 more source

Advantages and Challenges of Air-to-Air Missile Hypersonic Defense [PDF]

open access: yesHangkong bingqi, 2022
The change of war mode has led to the emergence of new threat targets. In recent years, with the development of technologies, air-space hypersonic flight technology continues to mature and form equipment.
Guo Zhengyu, Dong Meng, Du Miaomiao
doaj   +1 more source

Analysis of Hypersonic Platform-Borne SAR Imaging: A Physical Perspective

open access: yesRemote Sensing, 2021
The usage of a hypersonic platform for remote sensing application has promising prospects, especially for hypersonic platform-borne synthetic aperture radar (SAR) imaging.
Lihao Song   +6 more
doaj   +1 more source

Nonlinear Predictive Control with Sliding Mode for Hypersonic Vehicle

open access: yesInternational Journal of Aerospace Engineering, 2023
Hypersonic vehicles are difficult to control due to their rapid time variation, dynamic nonlinearity, strong coupling, and model uncertainty. This paper proposes a new nonlinear predictive controller to solve the problem.
Xiande Wu   +4 more
doaj   +1 more source

Nonequilibrium flow simulations using unified gas-kinetic wave-particle method [PDF]

open access: yesAIAA Journal 62 (4) (2024) 1411-1433, 2023
Nonequilibrium flows are common in aerospace engineering, and numerical simulations are vital in understanding non-equilibrium flow dynamics in spacecraft flight. The unified gas-kinetic wave-particle (UGKWP) method has been developed for multi-scale flow simulation, which models the coupled particle transport and collision within a numerical time in ...
arxiv   +1 more source

Influence Analysis of Simulation Parameters on Numerical Prediction of Compressible External Flow Field Based on NACA0012 Airfoil under Hypersonic Speed

open access: yesApplied Sciences, 2022
Currently, the influence of numerical parameters on the prediction accuracy of the compressible external flow field characterized by a NACA0012 airfoil under hypersonic speed, especially the influence analyses of the trailing edge shape, the modeling ...
Lu Yang, Guangming Zhang
doaj   +1 more source

Terminal Adaptive Guidance for Autonomous Hypersonic Strike Weapons via Reinforcement Learning [PDF]

open access: yes, 2021
An adaptive guidance system suitable for the terminal phase trajectory of a hypersonic strike weapon is optimized using reinforcement meta learning. The guidance system maps observations directly to commanded bank angle, angle of attack, and sideslip angle rates.
arxiv   +1 more source

High-enthalpy hypersonic flows

open access: yesAdvances in Aerodynamics, 2020
Nearly all illuminating classic hypersonic flow theories address aerodynamic phenomena as a perfect gas in the high-speed range and at the upper limit of continuum gas domain.
Joseph J. S. Shang, Hong Yan
doaj   +1 more source

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