1.

Find the geopotential height of an aircraft flying sea level where L0=-0.0065 k/m, p=30070.36Pa.a) 9120 kmb) 9144 kmc) 9854 kmd) 9874 km 8.The geopotential height in troposphere is given by __________

A. 9120 kmb) 9144 kmc) 9854 kmd) 9874 km 8.The geopotential height in troposphere is given by __________a) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)+1]
B. 9144 kmc) 9854 kmd) 9874 km 8.The geopotential height in troposphere is given by __________a) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)+1] b) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{L_0R}{g_0}\)-1]
C. 9854 kmd) 9874 km 8.The geopotential height in troposphere is given by __________a) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)+1] b) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{L_0R}{g_0}\)-1] c) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)-1]
D. 9874 km 8.The geopotential height in troposphere is given by __________a) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)+1] b) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{L_0R}{g_0}\)-1] c) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)-1] d) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{L_0R}{g_0}\)+1] View Answer
Answer» C. 9854 kmd) 9874 km 8.The geopotential height in troposphere is given by __________a) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)+1] b) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{L_0R}{g_0}\)-1] c) H=\(\frac{T_0}{l_0}\)[(\(\frac{p}{p_0}\))\(\frac{-L_0R}{g_0}\)-1]


Discussion

No Comment Found