AIAA-2019-3602: Design of a Modular Boundary Layer Bleed System for a Supersonic Wind Tunnel
Applied aerodynamics ; 2019 ; Dallas, TX
2019-01-01
8 pages
Conference paper
English
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Supersonic-inlet boundary-layer bleed flow
AIAA | 1996
|Supersonic-lnlet Boundary-Layer Bleed Flow
Online Contents | 1996
|Boundary layer bleed drag at supersonic speeds
TIBKAT | 1968
|Boundary Layer Bleed Drag at Supersonic Speeds
NTIS | 1968
|