1 atm = 2116 lb/ft2 = 1.01 × 105 N/m2. Calculate cp, cv, e, and h fora. The stagnation point of a high-speed missile are 934 ◦R and 7.8 atm, respectively.b. Air at standard sea level conditions

Q: Compute stagnation enthalpy of air at normal conditions (P=1atm, T=300K) moving with velocity of…

A: Write the equation for the stagnation enthalpy. h0=h+v22   =CpT+v22 Here, The stagnation enthalpy is…

Q: Nitrogen gas at a stagnation temperature of 300 K and a static pressure of 2 bar flows adiabatically…

A: Given: Stagnation temperature of nitrogen gas St=300 K Static pressure of nitrogen sp=2 bar The…

Q: 4.2. The ball catathermometer factor (F) is 620, time while the spirit column drops from 38 to 35°C…

A: Given   Catathermometer factor, F = 620 Temperature, T1 = 38oC                        T2 = 35oC Air…

Q: Suppose an aircraft is flying at standard sea-level at M = 0.8 and using a pitot-static tube for…

A: Given:The Mach number, The value of

Q: onsider an ideal nozzle of a rocket flying at an altitude where the ambient pressure and mperature…

A: 1) to calculate the nozzle supply pressure, throat area and mass flow rate at ambient pressure 2)…

Q: What is meant by the term “velocity of circulation” and explain its relevance in the quantity…

A: The quantity of money circulating in the economy during a specific time period is known as the…

Q: 1) What is the value of static temperature, stagnation temperature and stagnation pressure in the…

A: To calculatethe static temperature, stagnation temperature and stagnation pressure in the test…

Q: 4. A converging-diverging nozzle is designed for Mach Number, M = 2.0 at the exit. Air is supplied…

A: Given mech number at exit (me) = 2 Given pressure (P1)=900kpa Given temperature (T1)=500 k

Q: Air flows through a constant-area, insulated duct. At location 1, the conditions are Maj = 0.4, T; =…

A: Given: The mach number at location 1, Ma1 = 0.4 The mach number at location 2, Ma2 = 0.8 The…

Q: 1. An air flow with a Mach number of 2.0 passes through an oblique shock wave inclined at an angle…

A: Solution   Calculate the deflection angle α          tanα=2tanθM2sin2θ-1M2γ+cos2θ+2

Q: For Air: y = 1.4 Question B1 a) With the aid of sketches give a clear account of the operation of…

A: To calculate the mass flow rate, calculate area ratio, back pressure drawing

Conservation of Energy

In physics, the rule of the conservation of energy states that energy doesn’t disappear from the atmosphere; instead, it changes its form from one type to another. Energy is one of the most important physical quantities in nature, and it cannot be created or destroyed — only transformed.