Where are the statements then bbs lol
Answer:
k = 4.21 * 10⁻³(L/(mol.s))
Explanation:
We know that
k = Ae
------------------- euqation (1)
K= rate constant;
A = frequency factor = 4.36 10^11 M⁻¹s⁻¹;
E = activation energy = 93.1kJ/mol;
R= ideal gas constant = 8.314 J/mol.K;
T= temperature = 332 K;
Put values in equation 1.
k = 4.36*10¹¹(M⁻¹s⁻¹)e![^{[(-93.1*10^3)(J/mol)]/[(8.314)(J/mol.K)(332K)}](https://tex.z-dn.net/?f=%5E%7B%5B%28-93.1%2A10%5E3%29%28J%2Fmol%29%5D%2F%5B%288.314%29%28J%2Fmol.K%29%28332K%29%7D)
k = 4.2154 * 10⁻³(M⁻¹s⁻¹)
here M =mol/L
k = 4.21 * 10⁻³((mol/L)⁻¹s⁻¹)
or
k = 4.21 * 10⁻³((L/mol)s⁻¹)
or
k = 4.21 * 10⁻³(L/(mol.s))
Answer:d
Explanation:
Given
Temperature![=200^{\circ}\approc 473 K](https://tex.z-dn.net/?f=%3D200%5E%7B%5Ccirc%7D%5Capproc%20473%20K)
Also ![\gamma for air=1.4](https://tex.z-dn.net/?f=%5Cgamma%20for%20air%3D1.4)
R=287 J/kg
Flow will be In-compressible when Mach no.<0.32
Mach no.![=\frac{V}{\sqrt{\gamma RT}}](https://tex.z-dn.net/?f=%3D%5Cfrac%7BV%7D%7B%5Csqrt%7B%5Cgamma%20RT%7D%7D)
(a)![1000 km/h\approx 277.78 m/s](https://tex.z-dn.net/?f=1000%20km%2Fh%5Capprox%20277.78%20m%2Fs)
Mach no.![=\frac{277.78}{\sqrt{1.4\times 287\times 473}}](https://tex.z-dn.net/?f=%3D%5Cfrac%7B277.78%7D%7B%5Csqrt%7B1.4%5Ctimes%20287%5Ctimes%20473%7D%7D)
Mach no.=0.63
(b)![500 km/h\approx 138.89 m/s](https://tex.z-dn.net/?f=500%20km%2Fh%5Capprox%20138.89%20m%2Fs)
Mach no.![=\frac{138.89}{\sqrt{1.4\times 287\times 473}}](https://tex.z-dn.net/?f=%3D%5Cfrac%7B138.89%7D%7B%5Csqrt%7B1.4%5Ctimes%20287%5Ctimes%20473%7D%7D)
Mach no.=0.31
(c)![2000 km/h\approx 555.55 m/s](https://tex.z-dn.net/?f=2000%20km%2Fh%5Capprox%20555.55%20m%2Fs)
Mach no.![=\frac{555.55}{\sqrt{1.4\times 287\times 473}}](https://tex.z-dn.net/?f=%3D%5Cfrac%7B555.55%7D%7B%5Csqrt%7B1.4%5Ctimes%20287%5Ctimes%20473%7D%7D)
Mach no.=1.27
(d)![200 km/h\approx 55.55 m/s](https://tex.z-dn.net/?f=200%20km%2Fh%5Capprox%2055.55%20m%2Fs)
Mach no.![=\frac{55.55}{\sqrt{1.4\times 287\times 473}}](https://tex.z-dn.net/?f=%3D%5Cfrac%7B55.55%7D%7B%5Csqrt%7B1.4%5Ctimes%20287%5Ctimes%20473%7D%7D)
Mach no.=0.127
From above results it is clear that for Flow at velocity 200 km/h ,it will be incompressible.
Mass and chemical composition