Laboratory Section: ________ _ Score/Grade: __________ _ LAB EXERCISE Video b F). there is little heal because there are su few u10leculos oJ that allilude. The gases that make up air create pressure...

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Laboratory Section: ________ _ Score/Grade: __________ _ LAB EXERCISE Video b< ..="" ,,i,="" 10="" pit="" l,1li="" v11lro="" ~="" r="" http="" llgnn.gt/hz03sg="" earth's="" atmosphere:="" scan="" to="" view="" the="" pre•lab="" video="" temperature="" and="" pressure="" profiles="" the="" temperature="" of="" earth's="" atmosphere="" vudes="" greuuy="" with="" altitude.="" the="" average="" temperalw'e="" of="" earth's="" sw-face="" is="" 15°c="" (59°f),="" bn1="" tbe="" temperatllj'e="" of="" i.ha="" atmosphere="" dro_ps="" to="" -90°c="" (-130°f)="" and="" climbs="" lo="" uvor="" 1200°g="" (2200°f).="" these="" lemperatu:res="" are="" tl1e="" :msull="" of="" our="" atmosphere="" absorbing="" high-energy="" radi-="" ation="" from="" the="" slill.="" the="" ozoae="" layer="" converts="" 1ll1ra-="" vk)le1="" raclialion_="" to="" long-wave="" m.frared="" radiation,="" and.="" the="" ionosphere="" absorbs="" gbillma="" and="" x-ruy="" racliauon..="" while="" the="" temperature="" a1.="" the="" top="" of="" the="" atmuspltere="" is="" over="" 1200°c=""><>F). there is little heal because there are su few u10leculos oJ that allilude. The gases that make up air create pressure th.rough their motion, size. and number. This pressure is exortfici Oil aU surfaces in contaGI with Lhe air. 'The weigh I of Key Terms and Concepts Lhe Al mosphere, oi· air pressure, axerL~ an average force of approximately I kg/cm2 (14.7 lh/in2) at sea level. Under Lhe acceleraUon of gravity, air is com- pressed and therefore denser near Earth 's surface. The atmospbel'A rapidly thins with inr:reasecl alti- tude, a decrease tbal is measurable because air exerts Us weigh1 as pressure. Cunseguenlly, over half ilia total mass of the atmosphere is compressed below 5500 m (rn.uuo ft), 75% is compressed below 10,700 rn (35,105 fl) , llllcl 90% is compressed below 16.000 m (52,500 Et). All but 0.1% is beJow an alti- Ludu of 50,000 m (l63,6B0 ft). or 50 km (31 mi). In Lnb Exercise 10 we examine Earth's atmo- spht1ric temparalure and pressurn patterns. Lab Exercise 10 features three SP,ction.s. air pressure aneroid barometer barometer mesosphere standard ntmosphere stratopause llionnusphero tropopause troposphere mercury barometer mesopause ~EV s tralos phere thormopause conrApts After completion otthls lab, you should be able to: • Graph alt1tudlnal temperature changes In the atmosphere. • Demonstrate pressure trends with altitude. • Explain the standa~d atmosphere concept and plot key elements on a graph. • Locate a properly installed barometer (and, 1f necessary, a thermometer) and obtain data over a 3-day period, Materials/Sources Needed pencil culured p1molls Copyright© 2018 Pearson Educa1ion, Inc. calcu lator texthnok Lab Exercise 10: Earth's Atmosphere 75 I Applied Physical Geography: Geosystems in the Laboratory Lab Exercise and Activities Temperature Profile of tha Atmosoherfl lfasod on tom11Rmture. the atmusplwre is divided into four distinct zones 11r lovers: the thermospht!re, mesosphere, stratosphere, 1md tropos phere. Thu lrnnsilion a:rco al Lbe top of each touq;u1'nh1re region is naurnri using ll,e sulfi.x -pause, which means "Lu cause to change." i.e., thermopause, m.esopause, stralopause. und tropopause. Teinperaluros in Lhe lnwor atmosphere clo 1101 simply decline with altilude, for il is moro complex than this and actually varies. ln Iha upper atmo- sphere Lhe lflmporatw·e profilu shows that tempera- lures rise sharply in t.bt1 thormosphoro, up to 1wn~c: (2200°FJ and higher. However, womusl usf! diJJorenl concepts of "tomperaturo" and "heat" to unrlerstund I.his u[er.t. Tho intense rad int ion in lhls portion of the 11lmosphcro excites individual molocules (nitro- gen uncl oxygen) u11d atoms (u.xygen) to high levels of vilirotion. Tlilti kinetic P.nRrgy, llio energy ol motion, is the vibrational unu1-gy staled as "tempera- ture," However. tho density of L.he moletules is so low that littlo actual heul is produced. Heu ting in Lhe lownr almnsphurn nem· Ell1'th's sw•f11r.e differs bucrrnse t.be grflAler numhor nf moloc,dos in the• denser almosplrnre Lra:nsmil their kinetic energy as sensihle /uwr, moaning Uiat Wt! can senso it und mea- sure it. rlgurr 10 1 gives ynu Urn genernl trend rnr lhis lemperatmo prnfiJu that you specifically plul in thLc; section using rlata from Table 10.1. TABLE 10.1 Standard temperature values for the atmosphere Boundary of Atmosphere Altitude Temperature Therrnopa use 480 km (300 mi) I200°c (2200°F)+ Mesopause 80 km (50 rnl) -90°c (-130"F) Stratopause 50 km (31 rn1) o·c (32°n Tropopause 18km(11 mI) -57°C (-70°F) Surtace (No I lem1s.) Sea level 1 s•c (59°F) t. Using tho graph in l'igu re 10. I , plot Lhe stuntl11rd lemperatme values given in Toble L0.l. (Tho sea level value has boon rJ0 11e for yo11.) Allor yo11 plot Lhe rlAla points, counecl LhH1n with o line greph lo com- plete lbu profifo. Label UIB Layors or t.be almol'!pboro and llm b:ansilion areB.'l ut lhfl lop of eocb layer. Analysis uncl r.omplotion questions about tho standard lompornture profile. 2. Briefly explain why the tamporalure d0crouses A$ altitude lncreasos in tho lroposphero (at the normal lupl'IA rato). J. Why do tornperaturus Increase tliro11ghoul 111ost of 1110 slratosphorn? SpedJ1r.ally d.isctisA lhe process thal produces this warming llffoct. 76 Copy11ght l!ll 2018 Pearson Education, Inc 480 320 160 {:? 80 Q) -Q) E 0 ~ · 50 20 10 0 ' "- ' "',. '- I',. C0 -90° F0 - 130° -650 -400 -850 -400 Th ermopause - 15° 0° 5° 32° / V 5° 10° 15° 25° 41 ° 50° 59° 77° A Figure 10.1 Atmospheric temperature profile graph Copyright© 2.018 Pearson Education, Inc Lab Exercise 10: Earth's Atmosphere / 'v 400° 752° 300 200 -.... ' 100 -.... I".. 50 31 I',. I"- 12.4 6.2 0 800° 1200° 1472° 2190° 77 I Applied Physical Geography: Geosystems in the Laboratory 4 . Briefly explain why temperulutes increaso in Lhe lhermosphere. Air Pres uro Any instrumonl that moasures air prossure is cu lled a haromeler. One type of barometer usus a r.olumn of mercury I hat is coun terbalanced by lbe mass of surrou:nding air exerting an equivalent pressurfl on a vessel of mercury lo which the column is attached. The mercury barometer was developlald by Ev1mge- lista Torrir.elli in 1647. Mercury barometers are rarc:ly used in schools beca11Sfl of the toxicity of mercury. A more common lypfl of baromelor, the aneroid barometer, is a small chamber thal is partially emp- tied of air. sealed, and connected to 1:1 mechanism that is sensitive lo c-.hanges in air pressure. As nir prnssure varies, the mechanism responds. Altimetry is Lhe measurement of altitude using air pressure. A pressu.re u.lLimeter is an instrumenl that measures allilude basod on a strict relalionship betwecu air pressure and alLitude. Air pressure is meaRured within lhe altimeter by un aneroid h1uome1er capsu le, witb tho iustrmnent grad1rnted in increments of altitude. A pilot must r.onstantly adjust Uie altimotor, or "zero" lhe al timeter, during flight as atmospheric densities change with air lomperaturo. Anolher type of altimeter-a radar allimeler- seods anrl receives radJo wavelengths between the p lw10 and the ground to deteunino aJtltude. NonnaJ sea level p-ressure is expressed as 1 O l3.2 mb (millibars) of mercury (o way of expressing forco per square meler of surface area). Al sea level standard atmospheric pressure is exprnssed in several ways: • 14,7 ll,/in2 (pounds per square inch. or psi) • 29.9213 inches of mercury (in Hg) • l 013.250 millibars (mb) • 101.325 kilopasca.ls (1 kiJoposcal = 10 miUihors) Some convenient conversions are hel pful: • 1.0 in Hg= 33.87 mb = 25.40 mm llg = 0.49 lb/in1 • 1,0 mb = 0.0295 in Hg= 0.75 mm Hg= 0.0145 lb/in2 The standnrd atmosphere for pressure in millibHrs end uJlitude in kilunrnters is given in Table 10.2. This is used in the activity that follows lhe table. 78 Copyright C 2018 Pearson Education, Inc Lab Exercise 10: Earth's Atmosphere TABLE 10.2 Standard atmosphere for pressure and altitude Altitude (km) 0,00 a.so 1.00 I 50 2 00 2.50 3 00 4.00 5 00 6 .00 7.00 8 00 9.00 70 60 50 40 ~ ..... 30 ~ i 25 E 0 ~ 20 15 10 ,_ - - - 5 0 a 100 200 Pressure (mb) 101"3.25 954.61 898.76 845.59 795.01 746.91 701 21 616 60 540.48 472 17 411.05 356 51 308 00 ,- _,_ 300 400 500 Millibars Altitude (km) 10.00 12.00 14.00 16.00 18.00 20,00 25.00 30.00 35.00 40.00 50.00 60.00 10.00 r- --- 600 700 ,_ 800 Pressure (mb) - 900 264,99 t93.99 141 .70 103.52 75.65 55.29 25.49 11 .97 5.75 2.87 0.79 0.23 0.06 44 31 > 25 --- 12.4 6.2 0 1013.2 &. rigure 10.2 Atmospheric pressure profile graph-1he standard almosphere--from the surface to 70 km, Copyright <02018 pearson education. inc. 79 i applied physical geography: geosystems in the laboratory 1. using the graph in figure 10.2, plot the standai:d atmosphere of air pressm e decrease with altitude pre- sented i_n table 10.2. after comple ting the plot, connect the data points with a. line to complete the pres- sure profile of the atmosphere. the data points from 0 lo 5 km ere plolled for you. 2. the information in table pearson="" education.="" inc.="" 79="" i="" applied="" physical="" geography:="" geosystems="" in="" the="" laboratory="" 1.="" using="" the="" graph="" in="" figure="" 10.2,="" plot="" the="" standai:d="" atmosphere="" of="" air="" pressm="" e="" decrease="" with="" altitude="" pre-="" sented="" i_n="" table="" 10.2.="" after="" comple="" ting="" the="" plot,="" connect="" the="" data="" points="" with="" a.="" line="" to="" complete="" the="" pres-="" sure="" profile="" of="" the="" atmosphere.="" the="" data="" points="" from="" 0="" lo="" 5="" km="" ere="" plolled="" for="" you.="" 2.="" the="" information="" in="">
Sep 30, 2021
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