Total enthalpy
Replacing the given values,
Calculate the total temperature downstream of a real, level-4 technology nozzle knowing that T9-1,000 K, V9-1,250m/s and с/,,-1,300J/(kgK) Calculate the total temperature downstream of a real...
Calculate Tis downstream of a 2-stage cooled turbine made up of identical stages with -0.7 knowing T4 2,000K, 7 -1.3 and considering level 4 technology efficiencies. Calculate Tis downstream of a 2-stage cooled turbine made up of identical stages with -0.7 knowing T4 2,000K, 7 -1.3 and considering level 4 technology efficiencies.
Calculate the isentropic efficiency of a real, level 4-technology diffuser of an engine mounted in the airframe of a subsonic aircraft operating at Mach 0.8. Calculate the isentropic efficiency of a real, level 4-technology diffuser of an engine mounted in the airframe of a subsonic aircraft operating at Mach 0.8.
theres 4 total questions oare Was teR Mailed to these tive cardhoiders requesting intormation on the numbe time period. The data follow. Sick Days & Age iles 1,000's)K$1,000's) harges Cardholder 1.2 2.0 1.5 2.3 2.7 1.6 2.5 2.2 4.2 3.2 2.7 0.5 2.1 0.8 reA regression Analysis has been performed to estimate the model and the output is given. Regression Statistics Multiple R R Square Adjusted R Square ,19954 56026 0.31389 71405 tandard Error bservations ANOVA O 2019 01:41:34 A...
1. Calculate the primary NAAQS concentration limit for 502 in units of ug/m' at standard temperature and pressure (STP:T - 25*C, P = 1 atm). 2. Fuel X9-6000 is 95.8% efficient in an airplane engine. The unburned fuel leaves as VOCS in the exhaust. For each kg of fuel X9-6000 (Molecular Weight, MW-98), the engine exhausts 20 kg of gases (MW = 28 g/mol). What is the fraction of VOCs in the exhaust (ppm)? ncinerator burns 30 tonnes of plastic...