Aramjet is shown in supersonic flight. the total pressure recovery is nd 0.90 and the nozzle is u expanded (note that po po). nder. calculate (a) ram temperature and pressure ratios, tr and π (b) the total temperature at the combustor exit, ts in k and the corresponding τλ (c) exhaust velocity, v9, in m/s (d) pressure thrust as a fraction of nozzle momentum nv9n9 thrust, 1.e., (e) the propulsive efficiency of the ramjet, np (note that the nozzle is not perfectly expanded, so you need to calculate v9eft) (1) thrust-specific fuel consumption, tsfc, in mg/s/n and lbm/hr/lbf

-first use of geothermal energy occurred more than 10,000 years ago in north america by american paleo-indians

-the first industrial use of geothermal energy began near pisa, italy in late 18th century

-in 1904, italian scientist piero ginori conti invented the first geothermal electric power plant in which steam was used to generate the power

-with the above experiment, the first geothermal plant in usa started in 1922 with a capacity of 250 kilowatts

-however, in 1946 first ground-source geothermal heat pump installed at commonwealth building in portland, oregon

-during the 1960’s, pacific gas and electric began operation of first large scale geothermal power plant in san francisco, producing 11 megawatts

-in 1973, when oil crisis began many countries began looking for renewable energy sources and by 1980’s geothermal heat pumps (ghp) started gaining popularity in order to reduce heating and cooling costs

-as effect of climate change started showing results, governments of various countries joined hands to fight against it, for which kyoto protocol was signed in japan in 1997, laid out emission targets for rich countries and required that they transfer funds and technology to developing countries, 184 countries have ratified it

hope this

mass and volume are the answers you are looking for

because if the tool that you are using is not balanced it there would be false mass.