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Atmosphere
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11 December 2018

Correction: Teixeira, M.A.C. Diagnosing Lee Wave Rotor Onset Using a Linear Model Including a Boundary Layer. Atmosphere 2017, 8, 5

Department of Meteorology, University of Reading, Earley Gate, PO Box 243, Reading RG6 6BB, UK
This article belongs to the Special Issue Atmospheric Gravity Waves
The author would like to correct a published article by Teixeira [1], in which there is a factor of 2 missing from his Equation (24). The correct equation should read:
u 1 L ( z = 0 ) H U h 0 = 4 π a H k L h ^ ( k L ) sin ( k L x ) F r - 2 - n 2 ( k L ) cosh ( k L ) - k L sinh ( k L ) k L 1 + n 2 ( k L ) - 1 sinh k L + 1 + n 2 ( k L ) - F r - 2 cosh k L .
This implies that Equation (25) in [1] should be corrected to:
h 0 H crit = 1 4 π H a k L 2 1 + n 2 ( k L ) - 1 + 1 + n 2 ( k L ) - F r - 2 F r - 2 - n 2 ( k L ) k L | h ^ ( k L ) | F r - 2 - n 2 ( k L ) 2 - k L 2 .
As a consequence, Equation (27) of [1] should also be modified to:
D L = π ρ 0 k L | h ^ ( k L ) | U | min u 1 L ( z = 0 ) | ,
where, apart from removal of the factor of 2 on the right-hand side, a spurious factor of H has also been removed. The drag D L (per unit length) is now dimensionally correct. All other equations remain unchanged.
The results presented in Teixeira [1] remain qualitatively unchanged, but there are slight quantitative modifications to his Figures 1a,b, 4a,b, 7a,b, 8a,b and 9a,b, which display results from the inviscid model, expressed by his Equation (25), and the improved model expressed by his Equation (26), which also uses his Equation (25). These modifications amount to a value of the critical mountain height for flow stagnation that is twice smaller than in the original version, corresponding to contour values in the above-mentioned figures that are twice larger. Figures 1c, 2, 3, 4c, 5, 6, 7c,d, 8c,d and 9c,d of [1] are unchanged, because they result from the full model, which is correct and remains valid as originally formulated. The following figures, however, should replace those that were incorrect.
The conclusions presented in [1] remain unchanged. As in their original versions, the theoretical results presented in Figure 1a,b and Figure 2a still underestimate flow stagnation regions in parameter space considerably, whereas Figure 2b gives a fairly good description of flow stagnation, albeit showing some mismatches with the overlaid regime diagram. Figure 3a,b, Figure 4a,b and Figure 5a,b still give results that are qualitatively similar to their original versions, with the prediction of flow stagnation in Figure 4b and its absence in Figure 3a,b Figure 4a and Figure 5a,b for the relevant values of F r and a / H quoted in the captions of Figures 7–9 of [1].
Figure 1. (a) and (b) should replace Figure 1a,b in [1].
Figure 2. (a) and (b) should replace Figure 4a,b in [1].
Figure 3. (a) and (b) should replace Figure 7a,b in [1].
Figure 4. (a) and (b) should replace Figure 8a,b in [1].
Figure 5. (a) and (b) should replace Figure 9a,b in [1].
The author apologizes for any inconvenience this may have caused to the readers. The manuscript will be updated and the original will remain online on the article webpage, with a reference to this Correction.

Reference

  1. Teixeira, M.A.C. Diagnosing lee wave rotor onset using a linear model including a boundary layer. Atmosphere 2017, 8, 5. [Google Scholar] [CrossRef]

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