Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle (Shock Waves, 10.1007/s00193-015-0575-2) - Archive ouverte HAL Accéder directement au contenu
Article Dans Une Revue Shock Waves Année : 2016

Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle (Shock Waves, 10.1007/s00193-015-0575-2)

Résumé

Unfortunately, in the original online publication of the article there was a spelling mistake ‘schock’ in Fig. 1b. The corrected figure is given below. (Figure presented.)In Fig. 4 the word ‘section’ was missed. The corrected figure is give below.(Figure presented.) Figure 7 contained redundant text: “(a) Initial uniform mesh (50 elements) (b) adapted mesh”, which was also given in the figure caption. The corrected figure is given below.(Figure presented.) The original publication of the article has been updated to include the above corrected figures. Furthermore, in this article the subscript “k” is to be used to denote “Relative to the interaction zone” and the superscript “k” is to be used to denote “Relative to mode k.” Unfortunately, these were typeset inconsistently throughout the paper in multiple places, both in terms of font (roman/italic) and placement (subscript/superscript). The original publication of the article has been updated to ensure correct representation in this regard.

Dates et versions

hal-01367794 , version 1 (16-09-2016)

Identifiants

Citer

Nadir Bekka, Mohamed Sellam, Amer Chpoun. Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle (Shock Waves, 10.1007/s00193-015-0575-2). Shock Waves, 2016, 26 (4), pp.535--536. ⟨10.1007/s00193-016-0687-3⟩. ⟨hal-01367794⟩
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