Results 31 to 40 of about 6,012 (265)

Observations on some transonic wind tunnel test results of a standard model with a T-tail [PDF]

open access: yesScientific Technical Review, 2016
As a part of a periodic health monitoring of the wind tunnel structure, instrumentation and flow quality, a series of tests of an AGARD-C calibration model was performed in the 1.5 m T-38 trisonic wind tunnel of the Military Technical Institute (VTI) in ...
Damljanović Dijana   +4 more
doaj  

Experimental Investigation of the Flow, Noise, and Vibration Effect on the Construction and Design of Low-Speed Wind Tunnel Structure

open access: yesMachines, 2023
A wind tunnel is needed for a lot of research and model testing in the field of engineering design. Commercial wind tunnels are large and expensive, making them unsuitable for small-scale aerodynamic model testing.
Salem S. Abdel Aziz   +2 more
doaj   +1 more source

Study on Wind Load on the Topside Modules of Fixed Platforms

open access: yesShiyou jixie, 2020
The complex structure of the topside modules of the fixed platform makes it difficult to accurately calculate the wind load of the platform through a unified formula, and to consider the shadowing and interference effects between the platform modules. To
Zhu Benrui, Chen Guoming
doaj  

Preliminary Validation of the Wind Tunnel Based Flight Control System Evaluation Method

open access: yesMATEC Web of Conferences, 2018
As mathematical models of aircraft aerodynamics and rudder loadings always have to be built in the hardware-in-the-loop simulation, wind tunnel based flight control system (FCS) evaluation methods were proposed in order to test and evaluate the flight ...
Huang Min   +4 more
doaj   +1 more source

Aerodynamic Test of AGARD-B Model at Mach 10 in Arc-heated High-Enthalpy Wind Tunnel

open access: yes气体物理
The test capacity of hypersonic equipment is crucial to the development of hypersonic technology. However, the maximum Mach number simulated by conventional hypersonic wind tunnel is less than 10 currently due to the insufficient heater capacity ...
Tingting ZHANG   +4 more
doaj   +1 more source

Relativity Research of Total Pressure and Regulating Valve in Continuous Wind Tunnel and Its Application

open access: yesXibei Gongye Daxue Xuebao, 2020
As the main adjusting means of the total pressure for the continuous transonic wind tunnel, the characteristics of regulating valve directly affect the flow field performance of the wind tunnel, therefore, it is important to analyze and establish the ...

doaj   +1 more source

CFD and experimental data of closed-loop wind tunnel flow

open access: yesData in Brief, 2016
The data presented in this article were the basis for the study reported in the research articles entitled ‘A validated design methodology for a closed loop subsonic wind tunnel’ (Calautit et al., 2014) [1], which presented a systematic investigation ...
John Kaiser Calautit, Ben Richard Hughes
doaj   +1 more source

Field and Wind Tunnel Experiments of Wind Field Simulation in the Neutral Atmospheric Boundary Layer

open access: yesAtmosphere, 2022
To investigate the pollutant dispersion of a nuclear power plant, a field tracing experiment was carried out in neutral stratification weather with the main wind direction SSW.
Dong Xie   +5 more
doaj   +1 more source

TRAIL‐PEG‐Apt‐PLGA nanosystem as an aptamer‐targeted drug delivery system potential for triple‐negative breast cancer therapy using in vivo mouse model

open access: yesMolecular Oncology, EarlyView.
Aptamers are used both therapeutically and as targeting agents in cancer treatment. We developed an aptamer‐targeted PLGA–TRAIL nanosystem that exhibited superior therapeutic efficacy in NOD/SCID breast cancer models. This nanosystem represents a novel biotechnological drug candidate for suppressing resistance development in breast cancer.
Gulen Melike Demirbolat   +8 more
wiley   +1 more source

Selection criteria of optimal conditions for supersonic tests in a blowdown wind tunnel [PDF]

open access: yesScientific Technical Review, 2016
A natural desire of a wind tunnel test engineer is to plan and perform a test that will resemble the actual flight conditions as closely as possible. Geometric similarity and identical flight and wind tunnel Mach numbers are the primary requirements and ...
Damljanović Dijana, Vuković Đorđe
doaj  

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