Reynolds number influence on the backpressure-induced shock–boundary layer interaction in an asymmetric supersonic expansion flow-Reference-Cited by-同舟云学术

Reynolds number influence on the backpressure-induced shock–boundary layer interaction in an asymmetric supersonic expansion flow

Published:2019-04-17 Issue:2 Volume:2 Page:111-118
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Ji Yuan,He Miaosheng^ORCID,Liu Hong

Funder

Major Research Plan

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s42401-019-00025-x.pdf

Reference20 articles.

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3. Verma SB. Performance characteristics of an annular conical aerospike nozzle with freestream effect. In: 44th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, AIAA Paper 2008-5290. Hartford, CT

4. Schwane R, Hagemann G, Reijasse P. Plug nozzles-assessment of prediction methods for flow features and engine performance. In: 40th AIAA aerospace sciences meeting & exhibit, AIAA Paper 2002-0585. Reno, NV, USA

5. Onofri M, Calabro M, Hagemann G, Immich H, Sacher P, Nasuti F, Reijasse P. Plug nozzles: summary of flow features and engine performance - overview of RTO/AVT WG 10 subgroup 1. In: 40th AIAA aerospace sciences meeting & exhibit, AIAA Paper 2002-0584. Reno, NV, USA

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