Results 51 to 60 of about 441,039 (218)

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  

A Design and Construction of a Wind Tunnel for Engineering Laboratories [PDF]

open access: yesMATEC Web of Conferences, 2018
The propose of this research is to demonstrate a design and construction of a wind tunnel for engineering laboratories in order to study the principles and control wind speeds in the wind tunnel. In an experiment in aerodynamics and engineering, we found
U-tapao Chalida, Moryadee Seksun
doaj   +1 more source

Development of wind tunnel for laboratory wind turbine testing

open access: yes2011 North American Power Symposium, 2011
This paper presents the development of a wind tunnel that will be used for wind turbine testing in a controlled environment. The prototype is designed to be able to provide wind speeds of up to 20 m/s (∼43mph) depending on the cross sectional area of the tunnel chamber.
Dolan, Dale S.   +2 more
openaire   +4 more sources

The control system design and study for continuous supersonic wind tunnel

open access: yesXibei Gongye Daxue Xuebao, 2022
As the first continuous supersonic wind tunnel in China, Mach number and total pressure are the most important flow field parameters of the wind tunnel, how to precise control and rapid and stable adjustment of total pressure and Mach number is the key ...
CHEN Dan   +4 more
doaj   +1 more source

The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing

open access: yesJournal of Aerospace Technology and Management, 2014
This paper describes the update and characterization of a previously pure aerodynamics wind-tunnel into a facility able to simultaneously execute aerodynamics and aeroacoustics testing. It is demonstrated that the application of high-performance acoustic materials on strategic positions of the wind-tunnel circuit and punctual actions can substantially ...
Santana, Leandro Dantas   +3 more
openaire   +6 more sources

Wind Turbine Wake Modeling in Accelerating Wind Field: A Preliminary Study on a Two-Dimensional Hill

open access: yesFluids, 2019
Complex terrain can influence wind turbine wakes and wind speed profiles in a wind farm. Consequently, predicting the performance of wind turbines and energy production over complex terrain is more difficult than it is over flat terrain.
Omar M. A. M. Ibrahim   +3 more
doaj   +1 more source

Investigations of Wind Tunnel Wall Correction Methods for Airfoil Low-speed Dynamic Pressure Measurement

open access: yesHangkong gongcheng jinzhan, 2021
When the airfoil is subjected to unsteady wind tunnel test, it is necessary to correct the wall interference to obtain accurate aerodynamic data from test.Using a group of NACA 0012 airfoil models with same geometric similarities and different sizes ...
ZOU Hongyi, JIAO Yuqin, LIU Weibing
doaj   +1 more source

In wind tunnel the reproduction of vortex shedding behind circular cylinders at high Reynolds number regimes is incomplete [PDF]

open access: yesarXiv, 2023
Wind tunnel tests of 2D rough cylinders are presented. The goal is to simulate the alternate vortex shedding in flow regimes encountered in wind engineering applications, where the full scale Reynolds number is larger than the one that can be reproduced in wind tunnel with small scaled models.
arxiv  

Wind Tunnel Test of Subscale Ringsail and Disk-Gap-Band Parachutes

open access: yes, 2016
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients, as well as to capture the dynamic motions of a new Supersonic Ringsail parachute developed by the Low Density Supersonic Decelerator Project.
C. Zumwalt   +3 more
semanticscholar   +1 more source

Nano-ADEPT aeroloads wind tunnel test

open access: yesIEEE Aerospace Conference, 2016
A wind tunnel test of the Adaptable Deployable Entry and Placement Technology (ADEPT) was conducted in April 2015 at the US Army's 7×10 Foot Wind Tunnel located at NASA Ames Research Center.
B. Smith   +12 more
semanticscholar   +1 more source

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