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Boundary layer transition effects on flow separation around V/STOL engine inlets at high incidence (1984)

Salari, K. ; Wong, C. P. ; Chou, D. C. ; [et al.]

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Publication Date: 2019-06-28

Description: Numerical methods for calculating laminar and turbulent boundary layer development around vertical-short take off and landing engine inlets at high incidence angles are investigated. Various transition models were compared and evaluated in calculations off flow separation bound inside the inlet. Results of the transition effects on the boundary layer characteristics at onset of separation for two types of engine inlet geometries are presented. Some of the numerical results are compared with existing wind-tunnel test data for scaled inlet models to demonstrate the effects of transition models in the numerical scheme. The effects of transition modeling on the boundary layer development are illustrated for typical engine operating conditions.

Keywords: AERODYNAMICS

Type: AIAA PAPER 84-0432

Format: text

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