29.03.2016 Views

Nonlinear Fiber Optics - 4 ed. Agrawal

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

2.2. <strong>Fiber</strong> Modes 29<br />

across the core-cladding interface requires that Ẽ z , ˜H z , Ẽ φ , and ˜H φ be the same when<br />

ρ = a is approach<strong>ed</strong> from inside or outside the core. The equality of these field components<br />

at ρ = a leads to an eigenvalue equation whose solutions determine the propagation<br />

constant β for the fiber modes. Since the whole proc<strong>ed</strong>ure is well known [5]–[7],<br />

we write the eigenvalue equation directly:<br />

[ ][ J<br />

′<br />

m (pa)<br />

pJ m (pa) + K′ m(qa) J<br />

′<br />

m (pa)<br />

qK m (qa) pJ m (pa) + n2 c K ′ ] (<br />

m(qa) mβk0 (n 2 1<br />

n 2 =<br />

− ) 2 n2 c)<br />

1<br />

qK m (qa) an 1 p 2 q 2 , (2.2.8)<br />

where a prime denotes differentiation with respect to the argument and we us<strong>ed</strong> the<br />

important relation<br />

p 2 + q 2 =(n 2 1 − n 2 c)k 2 0. (2.2.9)<br />

The eigenvalue equation (2.2.8) in general has several solutions for β for each<br />

integer value of m. It is customary to express these solutions by β mn , where both<br />

m and n take integer values. Each eigenvalue β mn corresponds to one specific mode<br />

support<strong>ed</strong> by the fiber. The corresponding modal field distribution is obtain<strong>ed</strong> from Eq.<br />

(2.2.3). It turns out [5]–[7] that there are two types of fiber modes, designat<strong>ed</strong> as HE mn<br />

and EH mn .Form = 0, these modes are analogous to the transverse-electric (TE) and<br />

transverse-magnetic (TM) modes of a planar waveguide because the axial component<br />

of the electric field, or the magnetic field, vanishes. However, for m > 0, fiber modes<br />

become hybrid, i.e., all six components of the electromagnetic field are nonzero.<br />

2.2.2 Single-Mode Condition<br />

The number of modes support<strong>ed</strong> by a specific fiber at a given wavelength depends on<br />

its design parameters, namely the core radius a and the core-cladding index difference<br />

n 1 −n c . An important parameter for each mode is its cut-off frequency. This frequency<br />

is determin<strong>ed</strong> by the condition q = 0. The value of p when q = 0 for a given mode<br />

determines the cut-off frequency from Eq. (2.2.9). It is useful to define a normaliz<strong>ed</strong><br />

frequency V by the relation<br />

V = p c a = k 0 a(n 2 1 − n 2 c) 1/2 , (2.2.10)<br />

where p c is obtain<strong>ed</strong> from Eq. (2.2.9) by setting q = 0.<br />

The eigenvalue equation (2.2.8) can be us<strong>ed</strong> to determine the values of V at which<br />

different modes reach cut-off. The proc<strong>ed</strong>ure is complicat<strong>ed</strong>, but has been describ<strong>ed</strong><br />

in many texts [5]–[7]. Since we are interest<strong>ed</strong> mainly in single-mode fibers, we limit<br />

the discussion to the cut-off condition that allows the fiber to support only one mode.<br />

A single-mode fiber supports only the HE 11 mode, also referr<strong>ed</strong> to as the fundamental<br />

mode. All other modes are beyond cut-off if the parameter V < V c , where V c is the<br />

smallest solution of J 0 (V c )=0orV c ≈ 2.405. The actual value of V is a critical design<br />

parameter. Typically, microbending losses increase as V /V c becomes small. In practice,<br />

therefore, fibers are design<strong>ed</strong> such that V is close to V c . The cut-off wavelength<br />

λ c for single-mode fibers can be obtain<strong>ed</strong> by using k 0 = 2π/λ c and V = 2.405 in Eq.<br />

(2.2.10). For a typical value n 1 − n c = 0.005 for the index difference, λ c = 1.2 μm for<br />

a = 4 μm, indicating that such a fiber supports a single mode only for λ > 1.2 μm. In

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!