Affordable schlieren visualization methods for understanding three-dimensional supersonic flows
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s12650-020-00662-x.pdf
Reference27 articles.
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2. Brown YAI, Skews BW (2004) Three-dimensional effects on regular reflection in steady supersonic flows. Shock Waves 13:339–349
3. Bruce PJK, Burton DMF, Titchener NA, Babinsky H (2011a) Corner effect and separation in transonic channel flows. J Fluid Mech 679:247–262
4. Bruce PJK, Babinsky H, Tartinville B, Hirsch C (2011b) Corner effect and asymmetry in transonic channel flows. AIAA J 49(11):2382–2392
5. Carroll BF, Dutton JC (1992) Multiple normal shock wave/turbulent boundary-layer interactions. J Propul Power 8(2):441–448
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