Supersonic flow gradients at an overexpanded nozzle lip-Reference-Cited by-同舟云学术

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Supersonic flow gradients at an overexpanded nozzle lip

Published:2017-11-13 Issue:4 Volume:28 Page:765-784
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Silnikov M. V.,Chernyshov M. V.

Funder

Russian Foundation for Basic Research

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/article/10.1007/s00193-017-0772-2/fulltext.html

Reference33 articles.

1. Uskov, V.N., Chernyshov, M.V.: Differential characteristics of the flow field in a plane overexpanded jet in the vicinity of the nozzle lip. J. Appl. Mech. Tech. Phys. 47(3), 366–376 (2006). https://doi.org/10.1007/s10808-006-0064-6

2. Silnikov, M.V., Chernyshov, M.V., Uskov, V.N.: Two-dimensional over-expanded jet flow parameters in supersonic nozzle lip vicinity. Acta Astronaut. 97, 38–41 (2014). https://doi.org/10.1016/j.actaastro.2013.12.010

3. Saric, W.S.: Görtler vortices. Ann. Rev. Fluid Mech. 26(1), 379–409 (1994). https://doi.org/10.1146/annurev.fl.26.010194.002115

4. Sescu, A., Thompson, D.: On the excitation of Görtler vortices by distributed roughness elements. Theoret. Comput. Fluid Dyn. 29(1–2), 67–92 (2015). https://doi.org/10.1007/s00162-015-0340-2

5. Lucas, J.-M., Vermeersch, O., Arnal, D.: Transient growth of Görtler vortices in two-dimensional compressible boundary layers. Application to surface waviness. Eur. J. Mech. B/Fluids 50, 132–146 (2015). https://doi.org/10.1016/j.euromechflu.2014.11.005

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