REG NACA-TN-2738-1952 A probability analysis of the meteorological factors conducive to aircraft icing in the United States.pdf
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1、II ,_ZIt tNATIONAL ADVISORY COMMITTEEFOR AERONAUTICSTECHNICAL NOTE 2738 _/A PROBABILITY ANALYSIS OF THE METEOROLOGICALFACTORS CONDUCIVE TO AIRCRAFT ICINGIN THE UNITED STATES,By William Lewis and Norman R. BergrunAmes Aeronautical LaboratoryMoffett Field, Calif.WashingtonJuly 1952Provided by IHSNot f
2、or ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NATIONAL ADVISORY COMMITTEE FOR AERONAUTICSTECHNICAL NOTE 2738A PROBABILITY ANALYSIS OF THE METEOROLOGICALFACTORS CONDUCIVE
3、TO AIRCRAFT ICINGIN THE UNITED STATESBy William Lewis I and Norman R. Bergrun 2SUMMARYMeteorological icing data obtained in flight in the United Statesare analyzed statistically and methods are developed for the determina-tion of: (I) the various simultaneous combinations of the three basicicing par
4、ameters (liquid-water content, drop diameter, and temperature)which would have equal probability of being exceeded in flight in anyrandom icing encounter; and (2) the probability of exceeding any speci-fied group of values of liquid-water content associated simultaneouslywith temperature and drop-di
5、ameter values lying within specified ranges.The methods are particularly useful in the design of anti-icing equip-ment intended to bperate through the United States, to define simulta-neous combinations of the meteorological variables which could beencountered, and to ascertain the effectiveness of
6、the equipment inwithstanding the natural icing conditions to which it may be subjected.In addition_ a mathematical basis is provided for the future statisticalanalysis of meteorological icing data that might be obtained throughoutthe world.INTRODUCTIONThe program of research in aircraft ice preventi
7、on which has beenconducted by the NACA during the past several years has been directedprimarily toward the development of practical methods for the design ofthermal ice-prevention equipment for various airplane components. SinCea rational ice-prevention design requires a knowledge of the physicalcha
8、racteristics of icing conditions_ an important phase of the researchprogram has been an investigation of the meteorological conditions con-ducive to icing.The severity of an encounter with icing conditions is determinedprincipally by four factors; namely, the liquid-water content_ theiLewis Flight P
9、ropulsion Laboratory, NACA2Ames Aeronautical Laboratory, NACAProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2 NACATN 2738diameter of the drops, the temperature, and the horizontal extent of theconditions. The meteorological investigation has, theref
10、ore, been con-cerned with obtaining measurements of these quantities in a wide varietyof natural icing conditions in order to establish the range and rela-tive frequency of occurrence of various values, and combinations ofvalues, of these quantities.During the period 1945 through 1948, a considerabl
11、e amount of datawas collected by the Amesand Lewis Laboratories. These results_ anddiscussions of various phases of the investigation, have been reportedin references i through 4. All of these results_ together with similardata from observations made by other organizations_ were used as a basisfor a
12、 listing of estimated maximumicing conditions recommendedfor con-sideration in the design of anti-icing equipment (reference 5)- Theprobable maximumvalues listed in reference 5 were estimated on thebasis of what was considered a reasonable extrapolation from a limitedamount of data, and the concept
13、of the probability of encounteringvarious simultaneous combinations of values entered only in a subjectiveand qualitative way.In this report, the available data obtained in icing flights in theUnited States are analyzed statistically and the results are presentedgraphically in two forms. In the firs
14、t form, the results are plotted toshow the various combinations of liquid-water content, drop diameter,and ambient-air temperature which have equal probability of beingexceeded. In the second form, plots are presented to determine theprobability of exceeding any specified value of liquid-water conte
15、ntunder the condition that the value is associated simultaneously withvalues of temperature and drop diameter lying within specified intervals.Both plots are based on preselected values of horizontal extent; however,methods for estimating values applicable to other horizontal extents arealso present
16、ed.Although the results of this report are directly applicable only tothe United States, an estimation of the conditions prevailing in otherlocalities of similar climatic conditions can be made based upon theresults presented herein. As meteorological icing data are accumulatedfor regions outside th
17、e United States, the methods of this report shouldprovide a framework for placing the data on a statistical basis that isnot limited in scope to the United States.SYMBOLSThe following symbols are used throughout this report:A,B,C designation applied to three events occurring simultaneouslybut not ne
18、cessarily independentlyProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA TN 2738 3CDDcrADeFMtn0PPAPABCP (A)Pc(A,B)PePGchord length, feetmean-effective drop diameter, micronsthe smallest drop diameter for which drops will impinge upona thermal elem
19、entinterval of drop diameter, micronsNaperian base of logarithmscollection efficiency of an airfoil section_ percentfactor by which liquid-water-content values are multipliedto make them applicable to other distances of cloud hori-zontal extent, dimensionlessweight rate of water intercepted, pounds
20、per hour per footof airfoil spanan integeran icing condition considered to be defined by specificationsof the three variables, liquid-water content, temperaturedepression below freezing, and drop diameterprobability of overloading any given element of a thermalanti-icing systemprobability of the occ
21、urrence of event Aprobability of the simultaneous occurrence of threeevents, A, B, and Cprobability of the occurrence of event B, under the condi-tion that event A will occurprobability of the occurrence of event C under the condi-tion that both events A and B will occurprobability that any random i
22、cing encounter will be char-acterized by a combination of values of the variables(liquid-water content, temperature depression below freez-ing, and drop diameter), in which each variable must, res-pectively, equal or exceed a specified value of thatvariableprobability defined by the Gumbel probabili
23、ty distributionand expressed by equation (A1)Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4 NACATN 2738LkPi probability thatj for a random icing encounter, the followingthree conditions will simultaneously be fulfilled:(1) liquid-water content exc
24、eeding a specified value;(2) temperature within a specified interval; and (3) dropdiameter within a specified intervalprobability that drop diameter will have a value lying withina specified range (AD)probability that temperature will have a value lying withina specified range (AT)Pwi(AT)Qprobabilit
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