Artigo
Revisado por pares
Shock wave boundary layer interaction on suction side of compressor profile in single passage test section
2015; Springer Science+Business Media; Volume: 24; Issue: 6 Linguagem: Inglês
10.1007/s11630-015-0816-9
ISSN1993-033X
AutoresPaweł Flaszyński, Piotr Doerffer, Ryszard Szwaba, Piotr Kaczyński, Michał Piotrowicz,
Tópico(s)Aerodynamics and Fluid Dynamics Research
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