L = distance; M = mass; T = time; R = temperature
dimension(R) = L * (M * L/T^2) / (M * R) = [(L/T)^2]/R
dimension(RT) = (L/T)^2
dimension(sqrt(kRT)) = L/T (since k is dimensionless)
dimension(Nsqrt(kRT)) = L/T (since N is dimensionless)
dimension(F) = M*L/(T^2)
Therfore dimension of
= [M*L/(T^2)]/(L/T) = (M/T) = mass/time
It represents the change in mass of the rocket due to burning of rocket fuel.
It physically represents the mass flow rate.
Mass flow rate is the mass of a substance which passes through a given surface per unit of time.
Its unit is kiligram per second in SI i.e. kg/sec
help The thrust propelling a rocket is given by the equation where R is a gas...
Problem 2.3. An ideal ramjet is to fly at 20,000 ft with a Mach number of 3.5. The burner exit total temperature is to be 3200 °?? and the engine will use 145 lbm/s of air. The heating value of the fuel is 18,500 Btu/lbm. What is the diameter of the rounded exit, thrust, dimensionless thrust, and TSFC at this condition? (Assume that the temperature is 447.38°??, the static pressure is 6.747161 psia, and the specific heat ratio is 1.4...
A certain ideal rocket with a nozzle are ratio of 2.3 and a throat area of 5 sq. in. delivers gases at γ = 30 and R = 66 ft-lbf/lbm-⁰R at a chamber pressure of 300 psia and a constant chamber temperature of 5300 ⁰R against a back atmospheric pressure of 10 psia. By means of an appropriate valve arrangement, it is possible to throttle the propellant flow to the thrust chamber. Calculate and plot against pressure the following quantities...
The speed of sound in an ideal gas at a temperature T is given by c=sqrt{kRT} where T is in absolute units . For air, k=1.4 (dimensionless), R=0.06855 Btu/lbm-R . Find the speed of sound at T=530 R in mph (miles per hour).
Thornhill-Craver Equation The modified Thornhill-Craver Equation is used to calculate the gas flow rate through gas lift valves. The equation is 2 k+1 k k 155.5x C xAxP 2xgx up -r In this equation, qgas flow rate (MSCF/day) C discharge coefficient (dimensionless) A effective flow area (square inch) uupstream pressure (psi) P g gravitational acceleration (32.174 ft/s2) k ratio of specific heats (dimensionless) down (dimensionless) r s P. up down downstream pressure (psi) z gas compressiblity factor at the upstream...
Consider a turbofan engine with a bypass ratio of 6. The cruising Mach number is 0.85 at an altitude of 12000 m with an ambient temperature of 217 K. The ratio of stagnation pressure and ambient pressure for the fan and the core engine is 1.6. The stagnation temperature is 600 K at the exit of the core engine and 340 K at the exit of the fan. (a) If the fan and core streams expand in separate nozzles to...
The ideal gas law, discovered experimentally, is an equation of state that relates the observable state variables of the gas. pressure, temperature, and density (or quantity per volume$$ \eta V=N k_{\mathrm{B}} T(\mathrm{or} p V=n \mathrm{RT}) $$Where \(N\) is the number of atoms, \(n\) is the number of moles, and \(R\) and \(k_{\mathrm{B}}\) are ideal gas constants such that \(R=N_{\mathrm{A}} k_{\mathrm{B}}\), where \(N_{A}\) is Avogadro's number. In this problem. you should use Boltzmann's constant instead of the gas constant \(R\).Remaıkably. the...
The Ideal Gas Law 4 of 8 Review | Constants I Periodic Table The ideal gas law describes thee relationship among the pressure P. volume V. number of moles n and absolute temperature T'of an ideal gas Here is the relationship expressed mathematicaly Part A PV-nRT How many air molecules are in a 14.0 x 12.0 x 10.0 ft room (28.2 L 200 C and ideal behavior 1 ft? Assume atmospheric pressure of 1.00 atm a room temperature of where...
The Arrhenius equation for the dependence of the rate constant, k, on temperature is given by In k = + In A, where A is the frequency factor, R is the ideal gas constant, and EA is the activation energy. The rate of conversion of cyclo-propane to propene in gas phase was measured over the temperature range 750-900 K, and the rate constants that were found are reported below. Hint: think about what the following equation means In = (1,...
The van der Waals equation gives a relationship between the pressure p (atm), volume V(L), and temperature T(K) for a real gas: .2 where n is the number of moles, R 0.08206(L atm)(mol K) is the gas con- stant, and a (L- atm/mol-) and b (L/mol) are material constants. Determine the volume of 1.5 mol of nitrogen (a .39 L2 atm/mol2. b = 0.03913 L/mol) at temperature of 350 K and pressure of 70 atm.
The van der Waals equation...
Combined Gas Relationship Since the Ideal Gas Law produces a constant (R), it can be used to look at a gas sample in which initial and final conditions have changed. The combined gas relationship is as follows P.V R=P.V2 n, T n2 T2 where P, Vi,and T, and n, are the initial pressure, volume, temperature, and number of moles of gas. The final conditions are represented by P, V2, T2 and n2. If any of the conditions in the initial...