Results 21 to 30 of about 21,475 (198)

Effect of gas blowing on the head of thermal ablation vehicle

open access: yesAdvances in Aerodynamics, 2022
The reentry vehicle will encounter thermal ablation, especially at the stagnation point regime. A theoretical work has been done to analyze the thermal effect of gas blowing due to thermal ablation of surface material on the head of a general hypersonic ...
Qing Li   +3 more
doaj   +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 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

The aerodynamic wall [PDF]

open access: yesProceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2014
We study the trajectory of dense projectiles subjected to gravity and drag at large Reynolds number. We show that two types of trajectories can be observed: if the initial velocity is smaller than the terminal velocity of free fall, we observe the classical Galilean parabola: if it is larger, the projectile decelerates with an asymmetric trajectory ...
Cohen, Caroline   +5 more
openaire   +4 more sources

Warp drive aerodynamics

open access: yesJournal of High Energy Physics, 2022
Abstract In this work we analyse the potential for a warp drive spacetime to develop instabilities due to the presence of quantum matter. Particularly, we look for points of infinite blueshift (which are analogous to points of a black hole inner horizon, known for its semiclassical instability), and categorise them through the ...
Carlos Barceló   +4 more
openaire   +4 more sources

Research on Stall Characteristics of Droop Leading Edge Combined with Internal-blowing Flaps

open access: yesHangkong gongcheng jinzhan, 2022
The internally blown flap is of efficient lift enhancement ability,but stall angle of attack drops significantly at a higher jet momentum.In order to improve the stall characteristics,the stall characteristics of the internally blown flap with the droop ...
HE Meng, ZHANG Liu, ZHAO Lei, LI Chang
doaj   +1 more source

A decomposition formula for the wall heat flux of a compressible boundary layer

open access: yesAdvances in Aerodynamics, 2021
Understanding the generation mechanism of the heat flux is essential for the design of hypersonic vehicles. We proposed a novel formula to decompose the heat flux coefficient into the contributions of different terms by integrating the conservative ...
Dong Sun   +5 more
doaj   +1 more source

Nonlinear Modeling Study of Aerodynamic Characteristics of an X38-like Vehicle at Strong Viscous Interaction Regions

open access: yesEntropy, 2022
Strong viscous interaction and multiple flow regimes exist when vehicles fly at high altitude and high Mach number conditions. The Navier–Stokes(NS) solver is no longer applicable in the above situation.
Dingwu Jiang   +3 more
doaj   +1 more source

Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraft

open access: yesAdvances in Aerodynamics, 2019
How to solve the hypersonic aerothermodynamics around large-scale uncontrolled spacecraft during falling disintegrated process from outer space to earth, is the key to resolve the problems of the uncontrolled Tiangong-No.1 spacecraft reentry crash.
Zhi-Hui Li   +5 more
doaj   +1 more source

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