Design of a Modular Boundary Layer Bleed System for a Supersonic Wind Tunnel
AIAA Aviation 2019 Forum
2019-01-01
Conference paper
Electronic Resource
English
AIAA-2019-3602: Design of a Modular Boundary Layer Bleed System for a Supersonic Wind Tunnel
British Library Conference Proceedings | 2019
|Supersonic-lnlet Boundary-Layer Bleed Flow
Online Contents | 1996
|Supersonic-inlet boundary-layer bleed flow
AIAA | 1996
|Boundary layer bleed drag at supersonic speeds
TIBKAT | 1968
|Boundary Layer Bleed Drag at Supersonic Speeds
NTIS | 1968
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