J2071-1990

AERODYNAMIC TESTING OF ROAD VEHICLES


 

 

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标准号
J2071-1990
发布日期
1990年03月01日
实施日期
2013年02月12日
废止日期
中国标准分类号
/
国际标准分类号
/
发布单位
SAE - SAE International
引用标准
77
适用范围
As a simulation of road driving@ wind tunnel testing of full-size vehicles produces certain errors in the aerodynamic forces@ aerodynamic moments@ and surface pressures. The magnitude of these errors@ in general@ depends on the following: a. Flow quality b. Determination of the reference dynamic pressure c. Wind tunnel floor boundary layer d. Test section geometry and position of the car within that geometry e. Shape of the vehicle f. Blockage ratio: The ratio of the cross-sectional area of the vehicle to the cross-sectional area of the wind tunnel nozzle g. Wheel rotation h. Internal flow in the model The SAE Standards Committee@ Open Throat Wind Tunnel Adjustments had as a goal to document the knowledge of the influence of model interference on wind tunnel test results for automotive open jet wind tunnels. This document contains the following information related to this subject: a. Design data of open throat wind tunnels b. A summary of published and unpublished test data c. Documentation and theoretical explanation of various blockage correction procedures for automotive tests d. Critical evaluation of blockage correction procedures@ especially in relation to other influences@ such as test section geometry@ position of the car@ floor boundary layer@ etc. e. Recommendation of a calibration procedure to determine the effect of blockage and other influences in each individual wind tunnel An initial goal of the committee@ to recommend a well proven correction procedure for automotive open jet wind tunnels based on blockage theory (Figure 1)@ could not be established at this time. The reason is that@ besides blockage@ other factors@ such as test section geometry@ are at least as influential as pure blockage. As these influential parameters are wind tunnel specific@ a general valid adjustment procedure is presently not available. Clean Blockage means: ? no boundary layer effects ? no nozzle effects ? no collector/model interaction ? no buoyancy effects (i.e. longitudinal static pressure gradient)




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