if the % increase in power required for a helicopter to hover at an altitude above sea level is 6% higher that required to hover at sea level with the same figure of merit, determine the altitude. assume that the density change is 8% per km.
% power increase=6%
Let the power be x
New power =1.06x
"Density=\\frac{mass}{volume}"
Mass=density*volume
"\\frac{\\dot{W_{sea}}}{\\dot{W_{moun}}}=h\\sqrt{\\frac{\\rho_{moun}}{\\rho_{sea}}}"
"h=\\frac{\\dot{W_{sea}}}{\\dot{W_{moun}}}*\\frac{1}{\\sqrt{\\frac{\\rho_{moun}}{\\rho_{sea}}}}"
"h=1.06*\\frac{1}{\\sqrt{1.08}}"
"h=1.0200m"
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