Results 11 to 20 of about 4,354,998 (290)

Nonmalleable Information Flow Control [PDF]

open access: yesProceedings of the 2017 ACM SIGSAC Conference on Computer and Communications Security, 2017
Noninterference is a popular semantic security condition because it offers strong end-to-end guarantees, it is inherently compositional, and it can be enforced using a simple security type system. Unfortunately, it is too restrictive for real systems.
Ethan Cecchetti   +2 more
openaire   +1 more source

Comparative Study of Dynamic Stall between an Aircraft Airfoil and a Wind Turbine Airfoil in an Air–Particle Flow

open access: yesApplied Sciences, 2021
Dynamic stall in clean air flow has been well studied, but its exploration in air–particle (air–raindrop or air–sand) flow is still lacking. The aerodynamic performance loss of aircraft (NACA0012) and wind turbine (S809) airfoils and their differences ...
Junjun Jin   +4 more
doaj   +1 more source

Liquid information flow control

open access: yesProceedings of the ACM on Programming Languages, 2020
We present Lifty, a domain-specific language for data-centric applications that manipulate sensitive data. A Lifty programmer annotates the sources of sensitive data with declarative security policies, and the language statically and automatically verifies that the application handles the data according to the policies. Moreover, if verification fails,
Nadia Polikarpova   +5 more
openaire   +4 more sources

Active flutter suppression for a flexible wing model with trailing-edge circulation control via reinforcement learning

open access: yesAIP Advances, 2023
Previous attempts at active flutter suppression have been based on driving the deflection of multiple pairs of discontinuous mechanical control surfaces.
Zhen Chen   +4 more
doaj   +1 more source

Marking function of Stokes number on airfoils’ aerodynamic penalties in a gas–solid flow

open access: yesIET Renewable Power Generation, 2021
This paper aims to employ the Stokes number to mark aerodynamic penalties of airfoils caused by particles, which is crucial to implement their scaling experiments in a gas‐solid flow.
Junjun Jin   +4 more
doaj   +1 more source

Investigation of active flow control of jet deflection rate in passive secondary flow thrust vectoring nozzle

open access: yesAIP Advances, 2022
Jet deflection rate is an essential index in the research of thrust vector control technology. The vectoring deflection of the jet is an unsteady flow.
Shaoqing Chi   +3 more
doaj   +1 more source

Study on Characteristics of an AC Sliding Discharge Plasma Actuator Operating at Different Pressures

open access: yesActuators, 2023
Dielectric barrier discharge (DBD) has been one of the most promising techniques for flow control, but the practical application needs a large plasma surface.
Qijie Sun   +5 more
doaj   +1 more source

Experimental Investigation on Jet Vector Deflection Jumping Phenomenon of Coanda Effect Nozzle

open access: yesApplied Sciences, 2022
The Coanda effect nozzle is a fluid thrust vectoring technology that uses the Coanda effect to control jet vector deflection. The jumping phenomenon often occurs in the process of controlling jet vector deflection.
Shaoqing Chi, Yunsong Gu
doaj   +1 more source

Longitudinal flight dynamics modeling and a flight stability analysis of a monocopter

open access: yesAIP Advances, 2022
A monocopter, which is a biology-inspired aircraft based on the samara, has been proved to have passive flight stability. However, due to the asymmetry of its configurations and the constant rotation during flight, its flight dynamics equation is complex.
Shengxiang Tong   +3 more
doaj   +1 more source

Investigation of thrust vector angle control law based on micro-turbojet engine

open access: yesAIP Advances, 2022
The fluid thrust vectoring nozzle has a fixed profile, few moving parts, and lightweight structure, providing effective flight control for high maneuvering aircraft. The nonlinear control law of the jet deflection angle is one of the critical problems of
Shaoqing Chi   +3 more
doaj   +1 more source

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