Viscous Correction and Shock Reflection in Stunted Busemann Intakes

Author:

Ogawa H.,Shoesmith B.,Mölder S.,Timofeev E.

Publisher

Springer International Publishing

Reference14 articles.

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4. Mcnally, W.D.: BLAYER—Compressible laminar and turbulent boundary layers in arbitrary pressure gradients. Computer Program, LEW-11097, NASA Lewis Research Center (1994)

5. Metacomp Technologies Inc: CFD++. Software Package, Ver. 15.1 (2015)

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