Results 21 to 30 of about 116,768 (253)

A Review of Riemann Solvers for Hypersonic Flows [PDF]

open access: yesArchives of Computational Methods in Engineering, 2021
In the design of the hypersonic airliner which can greatly shorten the flight time and conduct space travel, it is of great significance for a Riemann solver to accurately simulate hypersonic flows. In this survey, the research process on the Riemann solver for hypersonic flows is reviewed, including the constructions of the traditional Riemann solvers,
Junqiang Bai   +3 more
openaire   +2 more sources

Shock Wave Intelligent Prediction Method for Hypersonic Vehicle

open access: yes气体物理, 2023
Accurate prediction of shock wave position of hypersonic aircrafts can effectively improve the accuracy and efficiency of computational fluid dynamics (CFD) simulation.
Yuan-hao ZHU   +6 more
doaj   +1 more source

Role of corner flow separation in unsteady dynamics of hypersonic flow over a double wedge geometry [PDF]

open access: yesPhysics of Fluids, 2021, 2021
This study investigates the origin and sustenance of self induced oscillations of shock structures in a hypersonic flow over a double wedge configuration. Previously, various researchers have considered the double wedge flow configuration for inviscid flow with variations of different inflows as well as geometric parameters such as inflow Mach number ,
arxiv   +1 more source

A Unified Asymptotic Theory of Supersonic, Transonic, and Hypersonic Far Fields

open access: yesAxioms, 2022
The problems of steady, inviscid, isentropic, irrotational supersonic plane flow passing a body with a small thickness ratio was solved by the linearized theory, which is a first approximation at and near the surface but fails at far fields from the body.
Lung-Jieh Yang, Chao-Kang Feng
doaj   +1 more source

Variant wing scheme and aerodynamic characteristics analysis of hypersonic vehicle

open access: yesHangkong gongcheng jinzhan, 2023
The variant aircraft can change its shape to adapt to different flight states and improve aerodynamic properties of aircraft. Aiming at a new hypersonic vehicle concept machine, the applicability of the wing variable sweep design on this hypersonic ...
ZHANG Xin   +5 more
doaj   +1 more source

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

Code-Verification Techniques for Hypersonic Reacting Flows in Thermochemical Nonequilibrium [PDF]

open access: yesJournal of Computational Physics, 425 (2021), 2020
The study of hypersonic flows and their underlying aerothermochemical reactions is particularly important in the design and analysis of vehicles exiting and reentering Earth's atmosphere. Computational physics codes can be employed to simulate these phenomena; however, verification of these codes is necessary to certify their credibility.
arxiv   +1 more source

A review of the mathematical modeling of equilibrium and nonequilibrium hypersonic flows

open access: yesAdvances in Aerodynamics, 2022
This paper systematically reviews the mathematical modeling based on the computational fluid dynamics (CFD) method of equilibrium and nonequilibrium hypersonic flows.
Wenqing Zhang   +3 more
doaj   +1 more source

Simulations of Hypersonic Boundary-Layer Transition over a Flat Plate with the Spalart-Allmaras One-Equation BCM Transitional Model

open access: yesMathematics, 2022
Transitional flow has a significant impact on vehicles operating at supersonic and hypersonic speeds. An economic way to simulate this problem is to use computational fluid dynamics (CFD) codes.
Yu Chen, Nick Gibbons
doaj   +1 more source

Electrical Discharges in Hypersonic Flows [PDF]

open access: yesThe Physics of Fluids, 1960
In order to study the interaction between an electrical current and a high-speed flow, experiments are being conducted with low-current electrical discharges in the 5 x 5-in. test section of the GALCIT hypersonic tunnel, in which continuous uniform flows are produced at M = 5.8 and total temperatures = 150°C.
Marlotte, Gary, Demetriades, A.
openaire   +4 more sources

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