Results 41 to 50 of about 2,387,085 (259)

Direct numerical simulation of supersonic and hypersonic turbulent boundary layers at moderate-high Reynolds numbers and isothermal wall condition

open access: yesJournal of Fluid Mechanics, 2022
We study the structure of high-speed zero-pressure-gradient turbulent boundary layers up to friction Reynolds number $Re_{\tau } \approx 2000$ using direct numerical simulation of the Navier–Stokes equations.
Michele Cogo   +3 more
semanticscholar   +1 more source

An Improved Method for Initial Sizing of Airbreathing Hypersonic Aircraft

open access: yesAerospace, 2023
One essential problem in aircraft conceptual design is initial sizing in which the aircraft primary parameters such as weight, size, and thrust are estimated for given design requirements.
Yalin Dai   +3 more
doaj   +1 more source

On the Görtler Vortex Instability Mechanism at Hypersonic Speeds [PDF]

open access: yesTheoretical and Computational Fluid Dynamics, 1989
The linear instability of the hypersonic boundary layer on a curved wall is considered. As a starting point the viscosity of the fluid is taken to be a linear function of temperature and real-gas effects are ignored. It is shown that the flow is susceptible to Gortler vortices and that they are trapped in the logarithmically thin adjustment layer in ...
Yibin Fu, Philip Hall
openaire   +2 more sources

Trajectory Estimation of Hypersonic Glide Vehicle Based on Analysis of Aerodynamic Performance

open access: yesXibei Gongye Daxue Xuebao, 2019
Due to high speed and high maneuverability of hypersonic glide vehicles (HGVs), the state estimation of such targets has always been a research hotspot.

doaj   +1 more source

Transitional hypersonic flow over slender cone/flare geometries

open access: yesJournal of Fluid Mechanics, 2022
Experiments are performed in a Mach-6 shock tunnel to examine the laminar-to-turbulent transition process associated with a sudden increase in surface angle on a slender body.
C. Butler, S. Laurence
semanticscholar   +1 more source

Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle

open access: yesInternational Journal of Aerospace Engineering, 2017
The Brazilian hypersonic scramjet aerospace vehicle 14-X B is a technological demonstrator of a hypersonic airbreathing propulsion system based on the supersonic combustion (scramjet) to be tested in flight into the Earth’s atmosphere at an altitude of ...
João Felipe de Araujo Martos   +5 more
doaj   +1 more source

Hydrocarbon Fuel Flow and Heat Transfer Investigation in Rotating Channels

open access: yesEnergies, 2023
Ram air turbines are used in the power generation systems of hypersonic vehicles, which can address the problem of the high power consumption of weapon systems.
Mengqiang Dong, Hongyan Huang
doaj   +1 more source

Stabilized detonation for hypersonic propulsion

open access: yesProceedings of the National Academy of Sciences of the United States of America, 2021
Significance There is now an intensifying international effort to develop robust propulsion systems for hypersonic and supersonic flight. Such a system would allow flight through our atmosphere at very high speeds and allow efficient entry and exit from ...
D. Rosato   +5 more
semanticscholar   +1 more source

Impact-Time-Control Guidance Law for Hypersonic Missiles in Terminal Phase

open access: yesIEEE Access, 2020
Recent researches on hypersonic vehicles adopted in military have gained a lot of interest because of its high flight speed and efficiency. However the guidance laws for hypersonic missiles against the anti-missile system to increase survivability and ...
Chenhao Zhu   +4 more
doaj   +1 more source

Nonlinear Conductive Graphene Composites for Pressure Sensing with a Linear Response and Voltage‐Driven Thermal Correction

open access: yesAdvanced Materials, EarlyView.
A nonlinear conductive graphene composite (NcGc) layer, incorporating a conductive laser‐reduced graphene oxide layer, is assembled into flexible pressure sensors without microstructural designs, achieving high sensitivity (742.3 kPa−1) and a wide linear sensing range (>800 kPa).
Feng Luo   +2 more
wiley   +1 more source

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