ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)最新文献

Multiple point dynamic gas density measurements using molecular Rayleigh scattering 多点动态气体密度测量使用分子瑞利散射

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-07-01 DOI: 10.1109/ICIASF.1999.827183

R. Seasholtz, J. Panda

引用次数: 6

Doppler global velocimetry: accuracy tests in a wind tunnel 多普勒全球测速:风洞精度测试

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827148

C. Lempereur, P. Barricau, JM. Mathé, A. Mignosi

引用次数: 7

New ONERA set-ups for the characterization of the resistance of materials to liquid and solid impacts 用于表征材料对液体和固体冲击的阻力的新ONERA装置

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827169

A. Deom, M. Lemistre, D. Balageas

{"title":"New ONERA set-ups for the characterization of the resistance of materials to liquid and solid impacts","authors":"A. Deom, M. Lemistre, D. Balageas","doi":"10.1109/ICIASF.1999.827169","DOIUrl":"https://doi.org/10.1109/ICIASF.1999.827169","url":null,"abstract":"ONERA has been involved in rain erosion studies since 1973. Rotating arms were used firstly to characterize the resistance of materials with droplet velocities in the range 200-300 m/s. In the 1990's, the Cavendish Laboratory developed a new apparatus, called MIJA (Multiple Impact Jet Apparatus), which can automatically produce water jets at high velocities. ONERA has been using a MIJA apparatus since 1994. The set-up was first validated in the range 200-300 m/s by comparison with rotating arm results. It is used now up to 600 m/s. The possibility of characterizing in-shape samples like radomes, as well as the determination of the influence of temperature and stress in the samples, were studied. A second water jet apparatus called SIJA, is in use since mid 1998. It allows rain erosion resistance measurements up to 1000 m/s. The possibility of characterization of material impact resistance was completed by another set-up called SPARC (Solid Particle Rebound Characterization apparatus) devoted to solid particle impact studies up to 190 m/s. Using two-dimensional laser velocimetry measurement, SPARC allows the determination of the angle and the velocity of rebound of a solid particle on a target.","PeriodicalId":291132,"journal":{"name":"ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)","volume":"73 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1999-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127585482","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 1

The recent methods for surface pressure and skin friction measurements on the models 模型表面压力和表面摩擦的最新测量方法

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827157

A. Bykov, V. Kulesh, A. Orlov, V. Pesetsky

引用次数: 1

Using of oscillatory conning experimental rig for separation of rotary and unsteady aerodynamic derivatives 利用振动锥实验装置分离旋转和非定常气动导数

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827177

A. Khrabrov, K. Kolinko, O. Miatov, J. Vinogradov, A. Zhuk

引用次数: 7

Pressure sensitive paint measurements on a wing model in a low-speed wind tunnel 在低速风洞中对机翼模型的压敏油漆测量

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827162

C. Klein, R. Engler, S. Fonov, O. Trinks

{"title":"Pressure sensitive paint measurements on a wing model in a low-speed wind tunnel","authors":"C. Klein, R. Engler, S. Fonov, O. Trinks","doi":"10.1109/ICIASF.1999.827162","DOIUrl":"https://doi.org/10.1109/ICIASF.1999.827162","url":null,"abstract":"Pressure field measurements on a wing profile are conducted to evaluate the accuracy of a measurement system using the so called \"binary\" or \"two-color\" Pressure Sensitive Paint (PSP) for low-speed (40-60 m/sec) environments. A part of the wing surface was coated with a binary paint. Two different light sources, a high pressure Xenon-flash lamp and a nitrogen laser were used for the excitation of the paint. The resulting fluorescence fields were acquired by a 16-bit CCD slow-scan camera. In front of this camera two different optical devices, a filter-shifting system or alternative a beam-splitting system, each of them were equipped with appropriate optical filters to separate the two different spectral emission wavelength of the paint, were used. Results shows that this optical pressure measurement system is able to resolve the small pressure changes on the model surface. Due to model movement and model deformation in between the image acquisition of the \"wind-off\" and \"wind-on\" images the necessity to use a binary paint for precise pressure measurements is clearly visible. These PSP-System working with binary paint can achieve pressure resolution in the region of 1 mbar.","PeriodicalId":291132,"journal":{"name":"ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1999-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122245423","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 4

Pressure sensitive paint for oscillating pressure fields measurements 用于振荡压力场测量的压敏涂料

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827164

S. Fonov, R. Engler, C. Klein, S. Mihailov, V. Mosharov, V. Kulesh, V. Radchenko

引用次数: 12

Laser anemometer measurements in a centrifugal compressor 激光风速计在离心压缩机中的测量

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827147

N. Saddour, A. Carrere

引用次数: 1

A comparative study of planar Mie and Rayleigh scattering for supersonic flowfield diagnostics 平面米氏散射与瑞利散射在超音速流场诊断中的比较研究

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827182

U. Brummund, B. Mesnier

{"title":"A comparative study of planar Mie and Rayleigh scattering for supersonic flowfield diagnostics","authors":"U. Brummund, B. Mesnier","doi":"10.1109/ICIASF.1999.827182","DOIUrl":"https://doi.org/10.1109/ICIASF.1999.827182","url":null,"abstract":"Planar Mie and Rayleigh scattering has been applied in a supersonic ramjet model combustion chamber (Scramjet chamber) which allows for the direct visualization of the fluid shear/mixing layer zone along the central axis of the combustion chamber. Hydrogen was injected parallel to the center line of the combustion chamber through holes at the base of an injector plate into a Mach 2.0 air flow. The evolution of shear/mixing layer downstream of the injector part has been visualized by laser light sheet scattering directly from the gas molecules (Rayleigh scattering) or from TiO/sub 2/ seed particles (Mie scattering). The laser-based optical techniques reveal details of the turbulent structure of the supersonic mixing process by single shot measurements and allow for the direct determination of the absolute visual shear/mixing layer thickness by averaged image processing. Compared to former experimental investigations applying the optical schlieren method significant smaller values of the absolute shear/mixing layer thickness have been measured by planar Rayleigh scattering and even smaller ones by planar Mie scattering. This difference is partly due to the different measurement techniques used and the different definitions of the shear/mixing layer thickness. Nevertheless the measured shear/mixing layer growth rates agree with previous results by other experimenters, confirming the compressibility effect of decreasing shear/mixing layer growth rates with increasing compressibility. Furthermore a slight but significant shear/mixing layer growth rate enhancement has been measured by shock/shear layer interactions.","PeriodicalId":291132,"journal":{"name":"ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1999-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115021300","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 4

Particle image velocimetry to quantify 3D-flow properties of gas turbine forced mixers 颗粒图像测速法量化燃气轮机强制混合器的三维流动特性

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) Pub Date : 1999-06-14 DOI: 10.1109/ICIASF.1999.827142

W. Scheuerpflug, N. Lawin

引用次数: 0