An airplane is operating from an airfield which has a barometric pressure of 26.81 in. Hg, and a runway temperature of 96.44 F. Calculate the temperature ratio. 0.9792 1.00223 O 1.0721 O 1.1864SPEED DENSITY PRESSURE TEMPER- TEMPER- OF KINEMTAIO ATLTITUDE FT RATIO RATIO ATURE ATURE RATIO SOUND VISCOSITY g KNOTS FT /SEC 1.0000 1.0000 1,0000 59.00 T.0000 661,7 .000158 1000 0.9711 0.9854 0.9644 65.43 0.9931 659.5 000161 SURE 2000 0.9428 0.9710 0.9208 51.87 0.9862 657.2 000165 3000 0.0151 0.9566 0.0962 48.30 0.9794 654.0 .000169 4000 0.8581 0.9424 0.8637 44.74 0.0725 652.6 .000174 0.8617 0.9283 0.8320 41.17 0.0656 650.3 .000178 6000 0.8359 0.9143 0.8014 37.60 0.0507 647.9 .000102 7000 0.8106 0.9004 0.7716 34.04 0.9519 645.6 .000187 8000 0.7860 0.8066 0.7428 30.47 0.9450 643.3 000192 0.7620 0.8720 0.7148 26.00 0:0301 640.9 000197 10000 0.7385 0.8593 0.6877 23,34 0.9312 638,6 .000202 15000 0.6292 0.7032 0.5643 5.51. 0.0969 626.7 000229 20000 0.5328 0.7299 0.4595 -12.32 0.8625 614.6 .000262 25000 0.4481 0.6694 0.3711 -30.15 0.8281 602.2 .000302 30000 0.3741 0.6117 0.2970 -47.90 0.7937 589.6 000349 35000 0.3090 0.5567 0.2353 -65.02 0.7504 576.8 000405 *36009 0.2971 0.5450 0,2234 -69.70 0.7519 573.8 000419 40000 0.2462 0.4062 0.1051 -69,70 0.7519 573.0 .000506 45000 0.1936 D.4400 0.1455 -69.70 0.7519 573.8 000643 50000 0.1522- 0.3002 0.1145 -60.70 0.7519 673.0 .000010 THE TROPOPAUSE