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本文(ASTM D5366-1996(2011) Standard Test Method for Determining the Dynamic Performance of a Wind Vane《风向标动力特性测定的标准试验方法》.pdf)为本站会员(terrorscript155)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASTM D5366-1996(2011) Standard Test Method for Determining the Dynamic Performance of a Wind Vane《风向标动力特性测定的标准试验方法》.pdf

1、Designation: D5366 96 (Reapproved 2011)Standard Test Method forDetermining the Dynamic Performance of a Wind Vane1This standard is issued under the fixed designation D5366; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year o

2、f last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This test method covers the determination of the startingthreshold, delay distance, and overshoot ratio of a wind va

3、nefrom direct measurements in a wind tunnel. This test method isapplicable only to wind vanes having measurable overshoot.1.2 This test method provides for determination of theperformance of a system consisting of a wind vane and itsassociated position-to-output transducer in wind tunnel flow.Use of

4、 values determined by this test method to describeperformance in atmospheric flow of a wind direction measur-ing system incorporating the vane must be done with anunderstanding of the differences between the two systems andthe two environments.1.3 This standard does not purport to address all of the

5、safety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Terminology2.1 Definitions:2.1.1 delay distance (D)the distance the

6、air flows past awind vane during the time it takes the vane to return to 50 %of the initial displacement.2.1.2 overshoot (un)the amplitude of a deflection of awind vane as it oscillates about uBafter release from an initialdisplacement.2.1.3 overshoot ratio (V)the ratio of two successiveovershoots,

7、as expressed by the equation:V5un11!/un(1)where unand u(n+1)are the n and n + 1 overshoots, respec-tively. In practice, since deflections after the first (to the sideopposite the release point are normally small, the initial releasepoint (that is, the n = 0 deflection) and the first deflection after

8、release (n = 1) are used in determining the overshoot ratio.2.1.4 starting threshold (Uo)the lowest speed at which thevane can be observed or measured moving from a 10 offset ina wind tunnel.2.2 Symbols:D (m) delay distanceUo(m/s) starting thresholdV (none) overshoot ratioh (none) damping ratiold(m)

9、 damped natural wavelengthun(degrees) overshoot; maximum angular excursionuo(degrees) reference directionuB(degrees) vane equilibrium positionuB uo(degrees) dynamic vane bias2.3 Calculated or Estimated Values:2.3.1 damping ratio (h)calculated from the overshootratio (1,2).2h5ln1/V!p21 ln1/V!#2!0.5(2

10、)2.3.2 damped natural wavelength (ld)at sea level in theU.S. Standard Atmosphere, damped natural wavelength isrelated to delay distance and damping ratio by the empiricalexpression (1,2).2ld5D6.0 2 2.4h!1 2h2!0.5(3)3. Summary of Test Method3.1 Reference Direction (uo, degrees) is the indicatedangula

11、r position of the vane when aligned along the centerlineof the wind tunnel.3.2 Vane Equilibrium Position (uB, degrees) is the finalresting position of the vane after motion in response to aninitial displacement. Ideally, uB= uo.3.3 Dynamic Vane Bias (uB uo, degrees) is the displace-ment of the vane

12、from the wind tunnel centerline at 5 m/s. Thismeasurement will identify wind vanes with unbalanced aero-dynamic response because of damage (for example, bent tail)or poor design.3.4 Starting Threshold (Uo, m/s) is determined by observ-ing or measuring the lowest speed at which the vane, releasedfrom

13、 a 10 offset position in a wind tunnel, moves toward uB.Movement must be distinguishable from vibration.3.5 Delay Distance (D, m) may be determined at a numberof wind speeds but shall include 5 m/s and 10 m/s. It iscomputed from the time required for the vane to reach 50 % ofthe initial displacement

14、 from 10 off uB. This time in seconds1This test method is under the jurisdiction of ASTM Committee D22 on AirQuality and is the direct responsibility of Subcommittee D22.11 on Meteorology.Current edition approved Oct. 1, 2011. Published October 2011. Originallyapproved in 1993. Last previous edition

15、 approved in 2007 as D5366 - 96(2007).DOI: 10.1520/D5366-96R11.2The boldface numbers in parentheses refer to the list of references at the end ofthis standard.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.is converted to delay dist

16、ance by multiplying by the windtunnel speed in metres per second. Tests shall include an equalnumber of displacements to each side of uB.3.6 Overshoot Ratio (V) may be determined at the sametime as the delay distance. The maximum angular excursion onthe opposite side of uBfrom the initial 10 displac

17、ement fromuBis measured. This value is divided by the initial displacementto obtain V.4. Significance and Use4.1 This test method will provide a standard for comparisonof wind vanes of different types. Specifications by regulatoryagencies and industrial societies (3-5) have stipulated perfor-mance v

18、alues. This test method provides an unambiguousmethod for measuring starting threshold, delay distance, andovershoot ratio.5. Apparatus5.1 Wind Tunnel (6):5.1.1 SizeThe wind tunnel shall be large enough so thatthe total projected area of supports, sensor apparatus, and thevane in its displaced posit

19、ion is less than 5 % of the cross-sectional area of its test section.5.1.2 Speed RangeThe wind tunnel shall have a speedcontrol that will allow the flow rate to be varied from 0 to atleast 10 m/s. The speed control shall maintain the flow ratewithin 60.2 m/s.5.1.3 Turbulence and SwirlAcross the volu

20、me to beoccupied by the vane, the flow profile shall vary by no morethan 1 % about the mean speed and shall exhibit a turbulenceof less than 1 %. (Warning Swirl in the wind tunnel mayinfluence starting threshold measurements. Variations in themeasurement of uBa low speeds likely indicate the existen

21、ce ofswirl.)5.1.4 CalibrationThe mean flow rate shall be verified atthe mandatory speeds of 5 and 10 m/s by use of transferstandards that have been calibrated by the National Institute ofStandards and Technology (formerly called the National Bu-reau of Standards)3or by a fundamental physical method.

22、5.1.4.1 Speeds below 2 m/s for threshold determinationshall be verified by a sensitive anemometer or by somefundamental time and distance technique, such as measuringthe transition time of smoke puffs, soap bubbles, or heat puffsbetween two points separated by a known distance.5.1.5 EnvironmentThe t

23、emperature and pressure of theenvironment within the wind tunnel test section shall bereported. Differences of greater than 3 % in the density of airwithin the test environment may result in poor inter-comparability of independent measurements of starting thresh-old, delay distance, and overshoot ra

24、tio since these values aredensity dependent.5.2 Measuring System:5.2.1 DirectionThe resolution of the wind vane position-tooutput transducer limits the resolution of the measure-ments. The accuracy of the positiontooutput conversion shallbe within 60.1. (WarningAvoid potentiometer dead spotsor cross

25、over positions while performing these procedures.)5.2.2 TimeThe resolution of time shall be consistent withthe distance accuracy required. For this reason, the timeresolution may be changed as the wind tunnel speed ischanged. For example, for a distance constant measurement to0.1 m, one must have a

26、time resolution of 0.05 s at 2 m/s and0.01 s at 10 m/s. If time accuracy is based on commercialelectrical power frequency, it will be at least an order ofmagnitude better than the resolution suggested above.5.3 Signal ConditioningCare shall be taken to avoidelectronic circuits in signal conditioning

27、 and recording devicesthat adversely affect the apparent vane performance.(WarningTime constants in signal conditioning and record-ing devices shall be less than 0.01 s.)5.4 Recording TechniquesThe measuring or recordingsystem shall represent the 10 displacement on each side of uBwith a resolution o

28、f 0.2. One simple technique is to use afast-response recorder (flat to 4060 Hz or better) with enoughgain so that a vane can be oriented in the wind tunnel with uBrepresented at mid-scale, and 610 of vane displacementtraversing the full span of the recorder.5.4.1 The recorder shall have a fast chart

29、 speed of 50 mm/sor more. An alternative is to use an FM tape recorder to recordthe signal. When played back at lower speed, a proportionatelyslower analog strip chart recorder yielding an equivalent50-mm/s chart speed is acceptable. Oscilloscopes with memoryand hard copy capability may also be used

30、.5.4.2 Digital recording and data reduction systems aresatisfactory if the sampling rate is at least 100 per second.6. Sampling6.1 Starting ThresholdTen consecutive tests at the samespeed meeting the test method requirement, five in eachdirection from uB, are required for a valid starting thresholdm

31、easurement.6.2 Delay Distance and Overshoot RatioThe arithmeticmean of ten tests, five in each direction from uB, is required fora valid measurement at each speed. The results of measure-ments at two or more speeds shall be averaged to a single valuefor delay distance and a single value for overshoo

32、t ratio.7. Procedure7.1 Dynamic Vane Bias:7.1.1 Set vane at tunnel centerline with no flow in the windtunnel.7.1.2 Adjust the wind tunnel to give a flow of 5 m/s.7.1.3 Measure the equilibrium vane position (uB) relative tothe tunnel centerline (uo). The angular difference, uB uois thedynamic vane bi

33、as.7.1.4 A dynamic vane bias greater than 1 indicates poordesign or a problem with the vane. Appropriate correctionsshall be made before continuing.7.2 Starting Threshold:7.2.1 Provide a mechanical method for holding and releas-ing the vane at 10 6 1 from uB. With no flow in the windtunnel, verify t

34、hat the vane moves by no more than 60.5 whenthe release mechanism is activated.3Available from National Institute of Standards and Technology (NIST), 100Bureau Dr., Stop 1070, Gaithersburg, MD 20899-1070, http:/www.nist.gov.D5366 96 (2011)27.2.2 Adjust the wind tunnel to a speed expected to be lower

35、than the starting threshold. Displace the vane by 10 and thenrelease it by the procedure described in 7.2.1. Observe themotion of the vane, if any, and record the angle, relative to uB,where motion ceases. Increase the speed slightly and repeat thetest; continue in this manner until a speed is reach

36、ed where thevane moves at least 1 toward uB.7.2.3 Using the speed determined in 7.2.2, displace the vaneby 10 and release it five consecutive times to one side of uB,observing and recording the angle where it stops each time.Repeat five times with the displacements to the other side ofuB.7.2.4 If al

37、l ten repetitions result in the vane moving at least1 toward uB, the wind speed may be used as the startingthreshold in accordance with this test method. The average ofthe absolute angular displacement from uBon each side shouldbe calculated. The higher of the two is the accuracy at thethreshold spe

38、ed.7.3 Delay Distance:7.3.1 Set the wind tunnel speed at 5 m/s. Displace the vane10 from uBand release it by the method in 7.2.1. Take fourmore samples in the same direction and five samples in theopposite direction.7.3.2 Repeat the procedure of 7.3.1 with the wind tunnelspeed set a 10 m/s.7.3.3 If

39、desired, repeat the procedure of 7.3.1 at other windtunnel speeds.7.3.4 For the ten samples taken at a tunnel speed, measurethe time from release to crossing 5 from uB(or 50 % of theactual release displacement, a nominal 10) for each of thesamples. Convert each of these times to a distance by multi-

40、plying by the tunnel speed. Average the distances to arrive at adelay distance for this speed.7.3.5 Repeat the procedure of 7.3.4 for ten samples taken ateach tunnel speed considered.7.3.6 Average the delay distances found in 7.3.4 and 7.3.5.The delay distance for each speed shall be within 10 % of

41、thisaverage.NOTE 1If the delay distance for any speed considered is outside610 % of the average, a delay distance for the vane cannot be specified.7.4 Overshoot Ratio:7.4.1 For each of the samples recorded for 7.3, read themaximum angular excursion on the opposite side of uBfromthe initial displacem

42、ent.7.4.2 Form a ratio by dividing each angular excursionobtained in 7.4.1 by the corresponding angular differencebetween the release angle and uB.Average these ratios to arriveat the overshoot ratio for the vane.8. Precision and Bias8.1 The accuracy in measurement of the wind tunnel speedlimits the

43、 accuracy of this test method. An accuracy of 0.1 m/sis required.This shall be documented at the wind tunnel facilityand be related to measurements at NIST5by a report on thetransfer standard that carries the same accuracy limit.8.2 PrecisionUsing this equipment and procedure, anestimate of the prec

44、ision of the test method follows:8.2.1 Starting ThresholdThe precision of this test methodis 0.1 m/s or better.8.2.2 Delay DistanceThe precision of this test method is0.1 m or better.8.2.3 Overshoot RatioThe precision of this test method is0.02 or better.8.3 Bias:8.3.1 Starting ThresholdThe bias of

45、this test method is nogreater than 0.15 m/s.8.3.2 Delay DistanceThe bias of this test method is nogreater than 0.15 m.8.3.3 Overshoot RatioThe bias of this test method is nogreater than 0.05.9. Keywords9.1 damping ratio; delay distance; overshoot ratio; startingthreshold; wind vaneREFERENCES(1) Fink

46、elstein, P. L., “Measuring the Dynamic Performance of WindVanes,” Journal of Applied Meteorology, Vol. 20, 1981, pp. 588594.(2) MacCready, Jr., P. B., and Jex, H. R., “Response Characteristics andMeteorological Utilization of Propeller and Vane Wind Sensors,”Journal of Applied Meteorology, Vol 3, No

47、. 2, 1964, p. 185.(3) “Determining Meteorological Information at Nuclear Power Facili-ties.” ANSI/ANS-3.11, American Nuclear Society, 2002 La GrangePark, IL.(4) Safety Theories, “Atmospheric Dispersion in Nuclear Power PlantSitingA Safety Guide,” International Atomic Energy Agency, No.50-FG-F3, 1980

48、.(5) U.S. Environmental Protection Agency, “Ambient Monitoring Guide-lines for Prevention of Significant Deterioration (PSD),” EPA-450/4-87-007, U.S. Environmental Protection Agency, 1987.(6) Pope, A., and Harper, J. J., Low-Speed Wind Tunnel Testing, JohnWiley and Sons, New York, 1966, pp. 85125; p

49、p. 406432.D5366 96 (2011)3ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are expressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and must be reviewed every five years andif not revised, either reapproved o

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