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Multi-Platform App-Embedded Model for Hybrid Air-Breathing Rocket Cycle Engine in Hypersonic Atmospheric Ascent – CORRIGENDUM

Published online by Cambridge University Press:  19 May 2022

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Abstract

Type
Corrigendum
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited.
Copyright
© The Author(s), 2022. Published by Cambridge University Press on behalf of Royal Aeronautical Society

In the original article, there is the same typo in the last equation in the set of Eq. (2) and (3) respectively. The authors and the publishers would like to apologise for this error. The correct equations are shown below.

(2) \begin{equation}T_{obl}=T_{1}\cdot\left[ \frac{(2+(\gamma-1)\cdot M_{n1}{}^{2})}{(\gamma+1)\cdot M_{n1}{}^2}\right] \cdot \left[1+\frac{2\cdot\gamma}{\gamma+1}\cdot(M_{n1}{}^{2}-1) \right]\quad\quad \to {\text{last equation of Eq}}{\rm{.}} \end{equation}
(3) \begin{equation}T_{2}=T_{obl}\cdot\left[ \frac{(2+(\gamma-1)\cdot M_{obl}{}^{2})}{(\gamma+1)\cdot {M}_{obl}{}^2}\right] \cdot \left[1+\frac{2\cdot\gamma}{\gamma+1}\cdot(M_{obl}{}^{2}-1) \right]\quad\quad \to {\text{last equation of Eq}}{\rm{.}} \end{equation}

References

Tsentis, S.E., Gkoutzamanis, V.G., Gaitanis, A.D., & Kalfas, A.I. (2021). Multi-platform app-embedded model for hybrid air-breathing rocket-cycle engine in hypersonic atmospheric ascent. The Aeronautical Journal, 125(1291), 16311653. doi: 10.1017/aer.2021.3 CrossRefGoogle Scholar
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