NASA NACA-TM-654-1932 Stresses Produced in Airplane Wings by Gusts《阵风在飞机机翼上产生的应力》.pdf
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1、a - N * NcTTht5 120112TECHII CAL MEORAiUMSNATI ONA ADVISORY COMIIiITTEE FOR AERONAUT I CS ISTRESSES PRODUCED IN AIRPLANE WINGS DY GUSTS By Hans Georg Kissner Zeitschrift fr P1ugtechni unci MotorlutscMfahrt Vol. 22, lbs. 19 and. 20, Oct. 14 and. 28, 1931 Verlag von R. 01d.erooiir, Munchen und Ber1iIA
2、/ -NAIIONAL TECHNICAL INFORMATION SERVICE - _ L - * 44 kIt aSgton SUDJECf TO CHA1GE Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NATIONAL ADVISORY COIMtTTEE POR ARONAUTICS TECICALMEMORAi1DUi. iTO. 654 STRESSES PRODUCED IN AIRPLANE Y1TGS 3Y.USTS*By
3、 Hans Georg Kussner Vhereas, in calm air,.: the strses in an airpl.ne wing depend on the airplane characteristics aid on the Di-lot, the latter has little or no influence on the magni-tude of such stresses in gusty weather from the point of view of mai.taining flight schedule an.d cruising seed. Con
4、seuently.,Uis airplane must be able. t.o withstand such strosse.s in any case. Ame irst infbrmation on stresses gusts was col-lectd by 7 Hoff in 1914* At that time there was no need to attach any special significance o.suchstreises, becai.se the speed range of the airplane, i.e., the ratio of maximu
5、m speed in uniform level flight to stalling speed was, in most cases, essentially lower than 2, and flying was, in the main, confiod to fair weather. But since that time the airplane has undergone onormous changes and improvements until to-day air traisportation has developed until it is practically
6、 ithperativo to fly under bad.as well as good. weather conditions.D In order prehensive conception of the flow phenomena in the open air, let us first glance over sone meteorological rep.ort: . 1. Official entry of telephone conversation with weather forecasting station, Tempelhof, Oct. 10, 1929: I
7、11At this station the following vertical components of gusts have been recorded: Normal (on cumulus clouds) . 2 Very frequently in bad weather zones, 6 Rare maxima, . . 12velocity 1f: to 4 ni/s to 8 rn/S ,q 13 ui/s i (Signed) Thalau. 3eanspruchung von Pl-igzeiigflgeln clurch Boen.“ Zeit-schrift fur
8、Flugtechnik und Motorluftschiffahrt, Oct. 14, 1931, pp. 579-586; and Oct. 28, 1931, pp. 605-615. *Tecilnische Berichte der Plugzeugmeisterei, Vol. 1, 1917, p. 61.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2 H.A.C.A. Technical Memoranthxrn-1o. :G
9、54 2. Letter from German Naval. Ober4iatory, Meteorolog-ical Research Institute, to the D.V.L O , October 25, 1929: “In answer ,toyour reQuest, we subrnit the latest reports- ofour forecasting station: - No exact measurements on the vertical velocity in :usts aie available at this post. 7e can only
10、give approximate values based. upon our xDeriences in numerous flights in clouds and. - gusts. - The most violent bumps are always ecountered at the front of an advancing gust roller, while at its upper border and above it the intensity is much abated In this respect only gust fronts with cold, air
11、inflow areas are beiig considered. - - “Theorder of magnitude. of the. vertical up and downward velocity doponentsvaries between 5 - and. 20 rn/s. . - - Sidling into or flying through a cumulus, the strongest gusts are encountered diectly at tie bordor of the cumulus; 5 to 10 rn/s may be con-sidered
12、. as normal for the vertical component of the velocity, Below the Cu. an up current of from 2 to 5 m/ prevails. In bad-weather zones Sto 10 m/s.velocities have been noted quite frequently. -Bad-weather zones adcornpanied by gusts are most generally bound. - up with areas of inflow of cold air and wi
13、th the passing of a convorgence.* 15 to 20 rn/s -are considered rare mximurn in gusts. However, it ay be assumed. that the maximum val-ues of the horizontal components in bad weather ma:. also be those for vertical gusts, so that an extreme of 30 rn/s is still within the ambit : po.ssiiility. - *500
14、 P. Exner, Dynamische Meteorologie, Leipzig, 1917, p. 2;9. V. Schmidt,. Tioncr Sitzungs Bericht, Vol. 119, 1910, Pu, 1J.Ol. .Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-IT.A.C.A. Technical Meruoranclurn io. 654 3 This information is deduced. from
15、 airplane meteor-ograph records. Th above experiences are con-firmed br aerological data from pilot ballobn ascensions. The figures cited. are valid for dynamic pressures within the first few kilome-tors abovo thc.ground.(Signed) Unterschrift. 3. A. Lohr, Cloud Plying:* The view of a convection cumu
16、lus field is much more imposing. Tho Cu. formations of the onvec- tion, space evince a much mightier formof towering head than the . Cu. of the friction space; they rise lofty into the sky and conjire, through their sharp contrast in light and shadow effect, miraculous, magnificent pictures. Towerin
17、g from their midst are lofty thund.erheads, reaching upward as high as 6000 meters, The pronounced bumpiness at the border of such towering heads is, of course, well known. But the warning against attempts to fly through them can- -not be emphasized enough. They are invested by ver-tical gusts of fr
18、om 10 to , l5 rn/s velocity, whereas beneath an ordin,ary Cu. formtt ion the uprush of the air is not expected to be more than 2 to 4 rn/s and which, of, late, is so successfully utilized in sai.-ing flight-. Closely related to the vertical current w.th up-wel.li:ng Cu. heads are the caps over the C
19、u. which toa. large tent are ice formations and risen stratus layers peiiotrated by the towering head. The latter spread, out and, often rise along the flanks of the tower., Prom time to time veil-like stratus clouds are pushed up by the turbulent layer beneath, making one feel as though being above
20、 a smooth stra-tus layer in which the umulus fields with soft fountain forms are imbedded. 0 “Another important object in cloud flying is the observation of the restlessness of the air within and in the neighborhood of clouds. One case in point is the restlessness of the air in the van of a gust. Ob
21、viously, flight within or below i.t is avoided. But frequently we stated ahead of the oncoming roller. It was found that in a spread of from 3 to 5 km in the van of the gust sorae very pronounced vertical *Ueteorologische Zeitschrift, 1930, September issue.Provided by IHSNot for ResaleNo reproductio
22、n or networking permitted without license from IHS-,-,-4 1T.A.C.A. Tec.nical ernorandm.ie,.554 gus:t,s ao exist which, however, vanish immediately aftor,ono passes directly above thb gust roller, where the spaco directly behind: the gust head, in Particular, is very calm.“ 0. Lange, The Aerological
23、ConditiOns in Cumulus Clouds : * “Although the entire descent was made with idling enine, the instrurnonts:r.ecodod piactically the same altitude for 20 seconds at 3000 motors, and a ajn of over 100 meters in 40 seond.s at 2500 meters, which can only be explained: as bei-ng due to vertical movements
24、 in the air. - The sinking velocity of the airplane from 4800 to .300.0metes is 540 meters per minu.te, and. from 2600 to 1200 meters, it is 530 me-ters per minute, or approxirate1y 9 rn/s. According to this., the upwind at 3000 metCrs is about 8 m/s, and. 12 rn/s at 2500 moters. I : b,etween, theve
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