Results 11 to 20 of about 61,014 (226)

FLEET Velocimetry for Aerodynamics

open access: yesAnnual Review of Fluid Mechanics, 2022
Long-lasting emission from femtosecond excitation of nitrogen-based flows shows promise as a useful mechanism for a molecular tagging velocimetry instrument. The technique, known as femtosecond laser electronic excitation tagging (FLEET), was invented at
P. Danehy   +4 more
semanticscholar   +1 more source

Numerical Simulation on Pyrolysis and Ablation Effects for Surface Material of Hypersonic Reentry Body

open access: yes气体物理, 2023
It is important to study the effects of pyrolysis and ablation of heat protection material in integrated design of hypersonic vehicles. In order to predict and assess the material pyrolysis and ablation effects on target signatures and microwave ...
Tie-suo GAO   +5 more
doaj   +1 more source

Learning aerodynamics with neural network

open access: yesScientific Reports, 2022
We propose a neural network (NN) architecture, the Element Spatial Convolution Neural Network (ESCNN), towards the airfoil lift coefficient prediction task.
W. Peng   +3 more
semanticscholar   +1 more source

Aerodynamics-assisted, efficient and scalable kirigami fog collectors

open access: yesNature Communications, 2021
To address the global water shortage crisis, one of the promising solutions is to collect freshwater from the environmental resources such as fog. However, the efficiency of conventional fog collectors remains low due to the viscous drag of fog-laden ...
Jing Li   +7 more
semanticscholar   +1 more source

Hypersonic aerodynamic force balance using temperature compensated semiconductor strain gauges

open access: yesAdvances in Aerodynamics, 2023
Metal foil strain gauges remain the state-of-the-art transducers for wind tunnel balances. While strain gauge technology is very mature, piezoresistive semiconductor sensors offer alternatives that are worth exploring to assess their unique benefits ...
Huacheng Qiu   +5 more
doaj   +1 more source

Numerical Study of Nonadiabatic Wall Effects on Aerodynamic Characteristics of CHN-T1 Standard Model

open access: yesAerospace, 2023
Cryogenic wind tunnels provide the for possibility aerodynamic tests to take place over high Reynolds numbers by operating at a low gas temperature to meet the real flight simulation requirements, especially for state-of-the-art large transport aircrafts.
Xiaobing Wang   +7 more
doaj   +1 more source

Unsteady Flow Driven by the Counter-Flow Jets of High-Altitude Engine Based on DSMC Simulation

open access: yes气体物理, 2023
Counter-flow engines are often used for aircraft slowing or separating. In order to study the interaction between the counter-flow jets and free stream at high altitudes, the rarefied flow driven by two counter-flow jets and hypersonic free stream was ...
Jun-lin WU   +4 more
doaj   +1 more source

Aerodynamics of Boundary Layer Ingesting Fuselage Fans

open access: yes, 2021
Boundary Layer Ingestion (BLI) potentially offers a large reduction in fuel burn and pollutant emissions. The Propulsive Fuselage Concept features an electrically driven fan at the aft section of the airframe that ingests 360◦ of the fuselage boundary ...
A. C. Pardo, C. Hall
semanticscholar   +1 more source

Numerical Investigation of Dorsal S-Shaped Inlet Flow Characteristic and Effects of Related Parameters

open access: yesXibei Gongye Daxue Xuebao, 2019
The air intake design system of the dorsal intake combined with the S-shaped inlet has been widely used in various combat aircraft due to its good stealth characteristics.

doaj   +1 more source

Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone

open access: yesAdvances in Aerodynamics, 2020
Properties of wall pressure beneath a transitional hypersonic boundary layer over a 7∘ half-angle blunt cone at angle of attack 6∘ are studied by Direct Numerical Simulation. The wall pressure has two distinct frequency peaks. The low-frequency peak with
Siwei Dong   +4 more
doaj   +1 more source

Home - About - Disclaimer - Privacy