Stokes wings

Taking into account all rotational lines of the Stokes and the anti-Stokes wing... 

Figure 6.8-10 Stokes wings of the collected rotational Raman spectra of N2 and O2 at room temperature using an argon ion laser.

Fig. 8. Luminescence spectra at T=10K of [Rh(thpy)2bpy]+ (upper trace) and of [Ir(thpy)2bpy] + (lower trace) doped into [Rh(ppy)2bpy] PF6. The inserts show the expanded origin region of the spectra. pws and pwa label the Stokes or Antistokes phonon wings, respectively, which accompany the origin line and the vibrational sidebands. The arrows mark two vibrations in the lr3+ spectrum without a counterpart in the spectrum of the corresponding Rh3 complex...

The absorption edge shifts to the blue (Fig. 1). The photoluminescence has a broad band peaking at 640 nm. The luminescence line shape is not Lorentzian and has a strong Stokes shift. Photoluminescence excitation (PLE) spectra have revealed a fine substructure of the band at its short-wave wing whose origin is attributed to the intrinsic luminescence contribution and to radiative recombination on defects. 

P. Hering, S.L. Cunba, K.L. Kompa, Coherent anti-Stokes Raman spectroscopy study of the energy paritioning in the Na(3P)-H2 collision pair with red wing excitation. J. Phys. Chem. 91, 5459 (1987)... 

So far, we have not imposed any constraints on the functions x = x(, r ) and y = y( ii), or their inverses = (x,y) and p = ri(x,y). One well-known transformation is Thompson s mapping, discussed in Thompson (1978, 1984), Thompson, Warsi, and Mastin (1985), White (1982), and Tamamidis and Assanis (1991). It was originally developed to solve the Navier-Stokes equations for viscous flows past planar airfoils, and later extended to three dimensions to study wing-fuselage effects in aerospace applications (Thomas, 1982). This method was also used in Chin (1992a,b 2001A,B) to study non-Newtonian flows in eccentric annuli and noncircular pipes. In Thompson s approach, (x,y) and r (x,y) are defined as solutions to the elliptic equations... 

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